Mixed Mode Testing of Fiber Reinforced Composites Using a Modified MMB Fixture (Englisch)
- Neue Suche nach: Chen, I.-J.
- Neue Suche nach: Golda, D.
- Neue Suche nach: Pelegri, A. A.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Neue Suche nach: American Society of Mechanical Engineers
- Neue Suche nach: American Society of Civil Engineers
- Neue Suche nach: Chen, I.-J.
- Neue Suche nach: Golda, D.
- Neue Suche nach: Pelegri, A. A.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Neue Suche nach: American Society of Mechanical Engineers
- Neue Suche nach: American Society of Civil Engineers
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ISBN:
- Aufsatz (Konferenz) / Print
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Titel:Mixed Mode Testing of Fiber Reinforced Composites Using a Modified MMB Fixture
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Beteiligte:Chen, I.-J. ( Autor:in ) / Golda, D. ( Autor:in ) / Pelegri, A. A. ( Autor:in ) / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers
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Kongress:41st, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference and exhibit; A collection of the 41st AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference and exhibit, AIAA/ASME/AHS adaptive structure forum, AIAA non-deterministic approaches forum, AIAA space inflatables forum, AIAA dynamics specialists conference ; 2000 ; Atlanta, GA
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Erschienen in:
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Verlag:
- Neue Suche nach: AIAA
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Erscheinungsdatum:01.01.2000
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Format / Umfang:8 pages
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Anmerkungen:In 5 vols, vol 1 in 3 pts; Papers
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ISBN:
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Medientyp:Aufsatz (Konferenz)
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Format:Print
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Sprache:Englisch
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Schlagwörter:
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Datenquelle:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Inhaltsverzeichnis Konferenzband
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 1
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Aircraft Aeroelastic Analysis and Design Using CFD-Based Unsteady LoadsKarpel, M. / Levy, Y. / Raveh, D. E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 3
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Structural Dynamics of Stiffened Plates Incorporating Piezoceramic Sensors and ActuatorsLeo, D. / Newbury, K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 3
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A Model for Generating Samples of Stationary Gaussian ProcessesGrigoriu, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 3
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Inflatable Sunshield in Space (ISIS) Versus Next Generation Space Telescope (NGST) Sunshield-A Mass Properties ComparisonCadogan, D. / Carey, J. / Goldstein, E. / Lou, M. / Pacini, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 3
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Coupling of Substructures for Dynamic Analyses: An OverviewCraig, R. R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 9
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New Developments in Computational Stochastic Mechanics - ApplicationsKeane, K. J. / Nair, P. B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 10
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Inflation Systems for Near-Term Space MissionsRoe, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 12
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Aeroelastic Tailoring of Empennage StructuresSensburg, O. / Tischler, V. A. / Venkayya, V. B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 13
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An Investigation of Piezoelectric Smart Composites Using a Coupled Piezoelectric-Mechanical ModelChattopadhyay, A. / Thornburgh, R. / Zhou, X. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 14
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Solar Concentrator Inflation Control SystemHancey, B. / Lester, D. / Siefkas, P. L. / Wassom, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 15
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Computational Structural Dynamics at General Motors CorporationNack, W. V. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 19
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Effect of Modal Test Statistics on Modeling Uncertainty and Model UpdatingAnderson, M. C. / Hasselman, T. K. / Li, X. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 23
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Concept Study of Membrane Tanks for Launch VehiclesIgawa, H. / Kasai, T. / Kimura, J. / Komatsu, K. / Ohyagi, T. / Sano, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 23
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Flexible Wing Model for Structural Wing Sizing and Multidisciplinary Design Optimization of a Strut-Braced WingGern, F. H. / Haftka, R. T. / Kapania, R. K. / Naghshineh-Pour, A. H. / Sulaeman, E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 24
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Impact Response of Adaptive Piezoelectric Laminated PlatesChristoforou, A. P. / Saravanos, D. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 24
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Multibody Dynamic Simulation of the Next Generation Space Telescope using Finite Elements and Fuzzy-SetsNoor, A. K. / Wasfy, T. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 26
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A Risk Assessment Approach for Fuselage Splices Containing MSD and CorrosionLiao, M. / Xiong, Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 28
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Inflatable Spacecraft using "Rigidization-on-Command" ConceptAllred, R. / Harrah, L. / Hoyt, A. / Lou, M. / McElroy, P. / Wise, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 33
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Structural Micro-Damage IndentificationChang, J. / Kim, N. / Lee, U. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 35
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Flutter Instability Tracking for Aeroelastic Design Optimization StudiesPidaparti, R. M. / Tischler, V. / Venkayya, V. B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 37
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Analysis and Ground Testing for Validation of the Inflatable Sunshield in Space (ISIS) ExperimentsAdams, M. / Alfano, J.-P. / Johnston, J. / Lienard, S. / Romanacci, P. / Stanley, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 37
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Robustness in Reliability-Based DesignMahadevan, S. / Stoebner, A. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 38
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Modal Truncation Vectors for Reduced Dynamic Substructure ModelsDickens, J. M. / Stroeve, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 43
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Active Aeroelastic Tailoring of High Aspect Ratio Composite WingsCesnik, C. E. S. / Ortega Morales, M. / Patil, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 44
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Damage Tolerance of Fiber Composite Airfoils with Piezoelectric Adaptive Control SystemAbdi, F. / Chamis, C. / Minnetyan, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 45
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Durability and Reliability Analysis for Flight Qualified Structural IntegrityAbdi, F. / Chamis, C. / DelMondo, F. / Latham, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 47
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X33 Transient Liftoff AnalysisBrunty, J. A. / Peck, J. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 48
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Modal Survey Test of SOTV 2X3 Meter Off-Axis Inflatable ConcentratorEngberg, R. / Lassiter, J. / McGee, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 51
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Development of an Analysis and Design Environment for Hybrid DampingArendsen, P. / de Boer, A. / Veul, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 54
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Dynamic Stochastic Crack Growth in Composites-A Challenge to the Research CommunityMaymon, G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 56
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Frequency-Shaping with Spatial CompensatorsClark, R. / Smith, G. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 57
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Characterizing Stability of Responses in a Nonlinear Aeroelastic SystemDowell, E. H. / Trickey, S. T. / Virgin, L. N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 59
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Ground Vibration Test Planning and Pre-Test Analysis for the X-33 VehicleBedrossian, H. / Hidalgo, H. / Tinker, M. L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 60
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Analytical Evaluation of Thermal Control Coatings for an Inflatable Solar Concentrator in Atmospheric and Thermal Vacuum ConditionsCadogan, D. / Malghan, S. / McElroy, P. / Wise, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 60
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Non-Deterministic Optimization - Composite Laminates and BladesAbumeri, G. / Chamis, C. / Kuguoglu, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 63
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A Methodology for Supersonic Panel Flutter Analysis of TPS SealsChen, R. R. / Cheng, G. / Mei, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 64
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Comparison of Dynamic Characteristics for an Inflatable Solar Concentrator in Atmospheric and Thermal-Vacuum ConditionsEngberg, R. / Lassiter, J. / Slade, K. / Tinker, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 67
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Static Shape Control of Composite Plates Using a Slope-Displacement Based AlgorithmChee, C. / Steven, G. / Tong, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 71
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On the Accuracy of Various Probabilistic MethodsFox, E. P. / Reh, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 72
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Nonlinear Thermoaeroelastic Modeling of Advanced Aircraft Wings Made of Functionally Graded MaterialsLibrescu, L. / Stere, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 76
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Wrinkling of an Inflated Membrane with Thermo-Elastic Boundary RestraintFitzgerald, D. / Jenkins, C. / Liu, X. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 78
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Modeling of Composite Beams with Integrated Piezoelectric Actuators: A Natural Mode ApproachGottlieb, J. J. / Hamdi, S. / Hansen, J. S. / Oguamanam, D. C. D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 80
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Modeling and Analysis of Fuzzy Systems Using Finite Element MethodRao, S. S. / Weintraub, P. N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 83
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An Innovative Structural Mode Selection Methodology: Application for the XH33 Launch Vehicle Finite Element ModelHidalgo, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 83
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Stress Singularities of Partially Constrained Interface Cracks in Anisotropic CompositesYin, W.-L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 84
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Robust Control and Active Vibration Suppression of a Flexible Composite StructureParker, G. / Robinett, R. / Starr, G. / Wilson, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 84
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Stability of Inflatable StructuresLennon, B. / Pellegrino, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 89
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Response Surface Based Fuzzy Analysis of Structural SystemsAkpan, U. O. / Koko, T. S. / Orisamolu, I. R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 93
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Motion Control of Adaptive Space Structures Based on Artificial Lagrange Energy MethodIkeda, T. / Kawamotuo, N. / Matsuzaki, Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 93
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Flutter Analysis of the X33Fowler, S. B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 94
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Integrally Stiffened Composite Structural Durability Evaluated by Computational SimulationAbdi, F. / Chamis, C. C. / Li, Q. / Minnetyan, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 94
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An Investigation of Geometric Imperfections in Parabolic Inflated Space StructuresNaboulsi, S. / Palazotto, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 100
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Evaluating the Convergence of Latin Hypercube SamplingManteufel, R. D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 101
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The Solar Parachute Concept for Solar Power Satellites and Solar SailsGreschik, G. / Mikulas, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 103
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A Strategy for Integrating a Large Finite Element Model: X-33 Lessons LearnedMcGhee, D. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 104
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Design & Testing of Multifunctional Structure Concept for SpacecraftHarris, N. / Morgenthaler, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 105
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Interlaminar Stress Analysis of Composite Laminates with Internal Ply-DropCho, M. / Kim, H. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 107
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The Material State Simulator: A PrototypeArwade, S. R. / Gigoriu, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 110
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Aeroelasticity and Dynamic Loads - From 1903 to the Supersonic EraFlomenhoft, H. I. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 111
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Design and Flight Testing of an Inflatable Sunshield for the NGSTAdams, M. / Culver, H. / Kaufman, D. / Lou, M. / Pacini, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 112
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Probabilistic Estimation of Pitting Corrosion Fatigue LifeMahadevan, S. / Shi, P. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 112
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Buckling Optimization of Composite Axisymmetric Cylindrical Shells under Uncertain Loading Combinationsde Faria, A. R. / Hansen, J. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 115
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Computer-Aided Optimal Placement and Sizing of Induced Strain Actuators for Broadband Structural ControlGiovanardi, M. / Pletner, B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 120
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Torus-Less Inflated Membrane Reflector with an Exact Parabolic CenterGreschik, G. / Mikulas, M. / Palisoc, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 123
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BMI Sandwich Wing Box Analysis and TestBush, H. / Mahler, M. A. / Palm, T. E. / Rouse, M. / Shah, C. / Wu, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 123
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Probabilistic Prediction of Fretting Fatigue Crack Nucleation Life of Riveted Lap JointsMahadevan, S. / Zhang, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 123
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Lessons Learned from Fixed and Rotary Wing Dynamic and Aeroelastic EncountersDonham, R. E. / Watts, G. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 124
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Active Structural Acoustic Control of Noise Transmission into a Cylindrical EnclosureClark, R. / Henry, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 130
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A Pressurized Deployment Model for Inflatable Space StructuresClem, A. / Main, J. / Smith, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 132
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Reliability Analysis of Creep-Fatigue FailureMahadevan, S. / Mao, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 132
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Thermally Induced Vibrations of an Internally Heated BeamBlandino, J. R. / Thornton, E. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 135
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Optimization of Piezoelectric Actuator Grouping for Aircraft Cabin Noise ControlGrewal, A. / Leigh, B. / Tse, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 141
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Pneumatic Envelopes: Poisson's Effect and Tendon Stiffness Drive Design DecisionsSchur, W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 141
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Delay of Creep Buckling and Probabilistic Failures of Linear Viscoelastic Plates Through Piezoelectric ControlBeldica, C. / Hilton, H. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 144
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Estimation of Response Amplitude Operators For Ships Via the Circular-Hyperbolic DecompositionHajj, M. R. / Nayfeh, A. H. / O'F Fahey, S. / Suleiman, B. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 145
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Structural Dynamics and Aeroelasticity of Rotary Wing AircraftLoewy, R. G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 150
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Block Toppling Model for Testing Against UncertaintyAkgun, M. A. / Haftka, R. T. / Nikolaidis, E. / Rosca, R. I. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 150
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Active Control of Vibration in Carbon Re-Enforced Composites Using Embedded Piezo-CeramicsGiovanardi, M. / Herrick, J. / Pletner, B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 152
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An Approximate Vibration Analysis of Curved PanelsAl-Jumaily, A. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 156
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Flight Control Using Distributed Shape-Change Effector ArraysGreen, L. / Montgomery, R. / Park, M. / Raney, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 158
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Static and Dynamic Analysis of Partially Wrinkled Membrane StructuresAdler, A. / Hedgepeth, J. / Mikulas, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 161
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Virtual Reality of Sound Generated from Vibrating StructuresKim, S. J. / Song, J. Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 166
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Adaption of Fast Fourier Transformations to Estimate the Structural Failure ProbabilityGrandhi, R. V. / Penmetsa, R. C. / Zhou, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 168
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Active Flow Control Using Microelectromechanical SystemsChen, P. / DeVoe, D. / Kiddy, J. / Kiger, K. / Niemczuk, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 172
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Design of a Membrane Mirror Using a Center PlungerAsh, J. / Jenkins, C. / Marker, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 172
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Coupled Transverse and Axial Vibration of a Compliant TowerBenaroya, H. / Han, S. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 176
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Some Early Cases of Servo-elastic InteractionsFlomenhoft, H. I. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 176
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Smart Air and Space Structure Demonstrations: Status and Technical IssuesCrowe, R. / Sater, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 180
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Life Prediction and Virtual TestingAbdi, F. / Chamis, C. / Farahmand, B. / Huang, D. / Jafroudi, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 182
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Response Surface Approximation of Non-Axisymmetric Features for Efficient Mechanical AnalysisMcMasters, M. / Seeley, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 185
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Early Uses of Electronic Computers in Aircraft Dynamic AnalysisBrenner, C. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 191
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Aeroelastic Oscillations of a Delta Wing with Piezoelectric StripsMateescu, D. / Misra, A. K. / Shrivastava, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 194
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Interfacial Micro-Level Stress Transfer in Macroscopic Thermoviscoelastic Creep of Unidirectional CompositesChung, P. W. / Namburu, R. R. / Tamma, K. K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 196
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Transient Load Analysis and Testing of QuikSCAT SpacecraftKuo, C.-P. / Vujcich, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 203
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Pioneer Rocketplane Reusable Launch SystemWolf, R. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 204
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Static Output Feedback Control of Nonlinear Aeroelastic Response of a Slender WingHodges, D. / Patil, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 205
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Review of Options for Structural Sensitivity CalculationsHaftka, R. T. / Qu, X. / van Keulen, F. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Comparison of Three Component Mode Synthesis Methods for Non-Proportionally Damped SystemsCraig, R. / Morgan, J. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 217
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Vibration and Dynamic Response Control of Elastically Tailored Nonuniform Adaptive Aircraft WingsLibrescu, L. / Na, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 219
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An Alternative Method for the Interface Modelling TechnologyAminpour, M. A. / Pageau, S. / Shin, Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 220
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Decoupled Second-Order Equations and Modal Analysis of a General Non-Conservative SystemPatil, M. J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 228
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Experimental Investigation of Delta Wing Active Flutter ControlClark, R. / Richard, R. / Rule, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 230
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Parallel Computations via a Single Anaysis Code of a Unified Family of Generalized Integration Operators (GlnO) for Non-linear Structural DynamicsKanapady, R. / Tamma, K. K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 232
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Error Estimation and Adaptivity in Three Dimensional p-version Finite Element AnalysisRavichandran, R. V. / Salagame, R. R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 237
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Recent Advances in Smart-Material Rotor Control ActuationGiurgiutiu, V. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 238
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A Predicted Newton-Raphson Iterative Algorithm Using Neural Network PredictionKim, J. H. / Kim, Y. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 241
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Dynamics Challenges of Saturn/ApolloRyan, R. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 248
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Development of and Adaptive Flexbeam for Rotorcraft Using Embedded Shape Memory Alloy (SMA) ActuatorsChopra, I. / Prahlad, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 249
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MAQSAT 3 on ARIANE 5 - The Structural Design of a Simulated Satellite with Tuneable PerformancesBurger, F. / Eder, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 249
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Some Structural Dynamics Contributions to the Apollo Program by the NASA Langley Research CenterPinson, L. D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 257
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ASTROS^* with Smart Structures and ASE Modules: Application to Flutter Suppression and Gust-Load AlleviationChattopadhyay, A. / Chen, P. C. / Liu, D. D. / Nam, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 258
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Saturn V Structural Dynamic Test/ModelingLawler, W. H. / Riley, G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 262
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Design and Experimental Testing of an Induced Shear Piezolectric Actuator for Rotor Blade Trailing Edge FlapsCentolanza, L. / Smith, E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 265
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Saturn V Thrust Buildup & Vehicle Release DynamicsGravitz, S. I. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 267
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Evaluation of Progressive Fracture in Composites at the Microstress LevelAbdi, F. / Chamis, C. / Minnetyan, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 273
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Closed-Loop Vibration Control Experiments on a Rotor with Blade Mounted ActuationHall, S. / Prechtl, E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 274
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Liquid Propellant Dynamics in the SATURN/APOLLO Vehicles - A Look BackAbramson, H. N. / Dodge, F. T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 274
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Stress Intensity Determination in Lap Joints with Mechanical FastenersCope, D. A. / Lacy, T. E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 283
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Apollo Lunar Module Landing DynamicsDoiron, H. H. / Zupp, G. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 284
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Incorporation of Temperature in Fatigue Models of PMC LaminatesUleck, K. R. / Vizzini, A. J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 288
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Vibration of Adaptive Wing-Rotor System for Tiltrotor Aircraft ApplicationKwon, H.-D. / Librescu, L. / Song, O. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 290
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An Equivalent Level of Safety Approach to Damage Tolerant Aircraft Structural DesignDu, J. / Lin, K. Y. / Rusk, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 294
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Twentieth Century Aeroelasticity of Bridges: Tacoma Narrows and BeyondScanlan, R. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 299
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Design and Realization of Frequency-Agile Piezoceramic TransducersBernard, J. / Lesieutre, G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 301
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Development of XF-2 Fighter Structures (Cocured Composite Wings)Kageyama, M. / Yoshida, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 303
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Inelastic Behavior of a 52-Story Building Subjected to Severe Ground ShakingVentura, C. E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 306
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Analysis and Design of High Frequency Periodically Layered IsolatorsLesieutre, G. A. / Smith, E. C. / Szefi, J. T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 314
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The Seismic Evaluation Process for Concrete Dams - Should It Be Updated?Duron, Z. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 316
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Actuator Power Reduction Using Tuned L-C Oscillator CircuitsChopra, I. / Sirohi, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 322
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Design Optimization of Stiffened Composite Panels for Damage ResistanceUbels, L. C. / Vercammen, R. W. A. / Wiggenraad, J. F. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 322
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A Parametric Study of a Flexible Ocean TowerBenaroya, H. / Kuchnicki, S. N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 328
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Modal Analysis and Optimization of the Offset Piezoceramic Stack ActuatorBayon de Noyer, M. / Hanagud, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 329
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Two-Dimensional Analysis on Unified Flutter Mechanism of Bridge DecksMahadevan, S. / Xiang, H. / Zhang, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 333
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Structural Information Technologies for Aircraft Design Process ImprovementTaylor, R. M. / Weisshaar, T. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 336
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Characterization of Microgravity Environment on MIRKaouk, M. / Kim, H. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 343
-
An Integrated Design and Analysis Tool for 3D Woven StructuresGoering, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 347
-
Microgravity Vibration Output Testing of Space Station Rotary JointsBoucher, R. L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 350
-
Multidisciplinary Design Tools for AffordabilityBlair, M. / Hartong, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 358
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General Dynamic Model Verification Procedure for Space Station Truss SegmentsChung, Y. T. / Foist, B. L. / Grau, E. / Sernaker, M. L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 361
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Composites Affordability InitiativeButler, B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 368
-
A Finite Element Thermal-Structural Analysis of the Mast of the International Space StationBigdeli, B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 371
-
A Comparison of Probabilistic and Lower Bound Methods for Predicting the Response of Buckling Sensitive StructuresArbocz, J. / Nemeth, M. P. / Starnes, J. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 379
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Estimation of the Transfer Function for the Russian Space Station Mir Due to Astronaut LoadsNeogi, N. / Newman, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 389
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Vibration Isolation Requirements for a Space Station Precision Deployable Structures LaboratoryDomber, J. L. / Peterson, L. D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 393
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Structural Similitude and Scaling Laws for Plates and ShellsRezaeepazhand, J. / Simitses, G. J. / Starnes, J. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 399
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A History of the Techniques and Equipment Used for Dynamic TestingLeifer, J. / Parkes, J. A. / Pusey, H. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 404
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A Dynamic Nonlinear Model of Multilayered Composite Shells Featuring Damaged InterfacesDi Sciuva, M. / Librescu, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 410
-
Temperature Dependent Modal Test/Analysis Correlation of X-34 Fastrac Composite Rocket NozzleBrown, A. M. / Davis, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 415
-
Bi-Stable Composite ShellsIqbal, K. / Pellegrino, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 417
-
On-Orbit Investigation of Transient Microdynamic Disturbances on a Deployed Truss StructureIngham, M. D. / Levine, M. B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 423
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Effects of Imperfections on the Buckling Response of Compression-Loaded Composite ShellsHilburger, M. W. / Starnes, J. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 428
-
A Method to Find Accurate Mass and Stiffness Matrices in System IdentificationMisawa, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 435
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Constraint Stabilization in Nonlinear Dynamics Via Control Theoretic MethodsFitz-Coy, N. G. / Kurdila, A. J. / McDaniel, D. E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 438
-
Performance of a Bell-Curve Based Evolutionary Optimization AlgorithmKincaid, R. K. / Sobieski, J. / Weber, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 443
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Explicit Equations of Motion for Constrained Mechanical Systems and New Directions in the Control of Nonlinear SystemsUdwadia, F. E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 447
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Damage Tolerant Topology Optimization under Multiple Load CasesAkgun, M. A. / Haftka, R. T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 451
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Multiresolution Methods for Representation of Volterra Series and Dynamical SystemsKurdila, A. J. / Prazenica, R. J. / Silva, W. / Strganac, T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 453
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Sequential Approximate Optimization Using Variable Fidelity Response Surface ApproximationsPadmanabhan, D. / Perez, V. M. / Renaud, J. E. / Rodriguez, J. F. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 461
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On the Modeling of Friction and Rolling in Flexible Multi-Body SystemsBauchau, O. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 464
-
Optimization of Trusses with Geometrically Nonlinear Response Using a Displacement Based ApproachGurdal, Z. / Missoum, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 470
-
Topology Optimization for Maximum Natural Frequency Using Simulated Annealing and Morphological RepresentationCui, G. Y. / Tai, K. / Wang, B. P. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 472
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Nonlinear Model Reduction of Structural Dynamic Aircraft ModelsKordt, M. / Lusebrink, H. / Schullerus, G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 480
-
Limit Cycle Oscillation Flight Test Results of a Fighter with External StoresDenegri, C. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 488
-
Nonlinear Model of the Flight of a Flexible AircraftPeronnet, J. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 492
-
Proper Orthogonal Decomposition Technique for the Computation of Nonlinear Panel ResponseBeran, P. S. / Mortara, S. A. / Slater, J. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 494
-
Buffet Simulation for the Kistler K-1 Launch VehicleBlelloch, P. / Coe, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 499
-
Limit Cycle Oscillation Prediction for Aeroelastic Systems with Continuous Non-linearitiesCooper, J. E. / Leung, A. Y. T. / Sedaghat, A. / Wright, J. R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 503
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Structural Dynamic Problems in Space Launch Vehicle Systems DevelopmentAcharya, A. R. / Singa-Rao, K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 508
-
Efficient Higher Order Shell Theory for Laminated Composites with Multiple DelaminationsCho, M. / Kim, J.-S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 514
-
Dynamic Behaviour of a Tethered System with Multi-Sub-Satellites in Elliptic OrbitsHiguchi, K. / Natori, M. C. / Okuizumi, N. / Takeichi, N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 519
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Stability of Delaminated Composite Plates Using a Higher Order TheoryChattopadhyay, A. / Radu, A. G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 523
-
X-34 Dynamic Modeling and CorrelationBlades, E. / Blelloch, P. / Dragone, T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 529
-
Failure Mechanism of Composite Laminates with Different Size Multiple Delaminations Subject to Compressive LoadSuemasu, H. / Wakabayashi, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 531
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Captive Carry Flutter Analysis for the X-34 Reusable Launch VehicleBlades, E. L. / Redgrave, G. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 539
-
Effect of Z-Pinning on Buckling of Delaminated Sandwich BeamsIfju, P. G. / Sankar, B. V. / Wallace, B. T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 542
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Effect of Area Formulations in Compressible Fluid-Structure InteractionKim, M. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 545
-
Mixed Mode Testing of Fiber Reinforced Composites Using a Modified MMB FixtureChen, I.-J. / Golda, D. / Pelegri, A. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 553
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Timoshenko-like Modeling of Initially Curved/Twisted Composite Beams with Oblique Cross-sectionsCesnik, C. E. S. / Hodges, D. / Volovoi, V. / Yu, W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 565
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The NEAR and MESSENGER Spacecraft: Two Approaches to Structure and Propulsion DesignHartka, T. / Mosher, L. E. / Persons, D. F. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 575
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The Interplay Between Hardware and Control System Design in the Development of the Active Rack Isolation SystemFialho, I. / Thampi, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 584
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Design and Testing of Reduced-Stiffness Umbilicals for Space Station Microgravity IsolationEdberg, D. L. / Wilson, B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 592
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Mechanism Design Principles for Optical-Precision, Deployable InstrumentsHachkowski, M. R. / Lake, M. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 601
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A Commerical Ready, High Reliable and High Producible RWA DesignFletcher, M. / Marshall, T. / Zuckerbrow, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 610
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Modal Scheduling and Switching SystemsFitz-Coy, N. / McDaniel, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 619
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Can Time Delays Be Useful in the Control of Structural Systems?Udwadia, F. E. / von Bremen, H. F. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 627
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The Design of a Toroidal Rubber SpringGlikman, Z. / Putter, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 633
-
Large-Scale Structural Analysis by Parallel Multifrontal Solver Through Internet PC'sKim, J. H. / Kim, S. J. / Lee, C. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 642
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Computational Schemes for Nonlinear Elasto-DynamicsBauchau, O. A. / Joo, T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 653
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Contact Conditions for Cylindrical, Prismatic, and Screw Joints in Flexible Multi-Body SystemsBauchau, O. A. / Bottasso, C. L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 664
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Adaptive Multi-modal Vibration Control of Wing-like Composite Structure Using Adaptive PPFHan, J.-H. / Lee, I. / Rew, K.-H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 674
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Acoustic Control of a Rocket Fairing Using Spatially Weighted Transducer ArraysClark, R. L. / Griffin, S. F. / Kemp, J. D. / Lane, S. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 680
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Control of a Class of Multidimensional Second Order Systems with Periodic CoefficientsDeshmukh, V. / Sinha, S. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 691
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Comparison of Active and Passive Suppressions of Nonlinear Panel Flutter Using Finite Element MethodKim, S. J. / Lee, S. K. / Moon, S. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 700
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Primary Sandwich Structure: A Unitized ApproachSchmidt, R. / Sheahen, P. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 708
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An Elementary Model for Structural DynamicsRehfield, L. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 719
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Static and Vibration Analyses of General Wing Structures Using Equivalent Plate ModelsKapania, R. K. / Liu, Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 735
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New Approaches for Obtaining Dynamic Modal Contribution Factor of Structural ResponsesHernandez, S. / Romera, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 741
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Innovative Passive Mechanisms for Control of Sound in a Launch Vehicle FairingClark, R. L. / Griffin, S. / Gussy, J. / Kemp, J. D. / Lane, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 749
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Validation of Structural Dynamics Models at Los Alamos National LaboratoryDoebling, S. W. / Hemez, F. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 764
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A Dynamic Finite Element (DFE) Formulation for Coupled Flap-Lab Vibrations of Propeller BladesGolnaraghi, M. F. / Hashemi, S. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 773
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Reduced-Order Modeling for Flutter PredictionBeran, P. S. / Pettit, C. L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 784
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Energy Based Design and Analysis of Staggered Solvers for Nonlinear Transient Aeroelastic ProblemsFarhat, C. / Piperno, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 799
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On the Importance of Aerodynamic and Structural Geometric Nonlinearities on Aeroelastic Behavior of High-Aspect-Ratio WingsHodges, D. / Patil, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 810
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Improving the Aerodynamic Approximation in Linear AeroelasticityGiri, J. / Hartley, D. / Jadic, I. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 819
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Aeroservoelastic Structural and Control Optimization Using Classical and Modern Robust Design SchemesIdan, M. / Karpel, M. / Moulin, B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 829
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Global-Local Analysis and Optimization of a Composite Tilt-Rotor WingClements, T. M. / Rais-Rohani, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 839
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Secondary Buckling of Laminated Composite PlatesHyer, M. W. / Tiwari, N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 850
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A Comparison of Three Algorithms for Tracing Nonlinear Equilibrium Paths of Structural SystemsGurdal, Z. / Ragon, S. A. / Watson, L. T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 861
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Controlling a Nonlinear Solution Procedure During a Progressive Failure AnalysisBrogan, F. A. / Knight, N. F. / Rankin, C. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 872
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Effect of Residual Stresses on Buckling Localization in a Cylindrical PanelNeedleman, A. / Tvergaard, V. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 879
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Inclusions in Ti-6Al-4V Investment CastingsClark, L. / Cotton, J. / Reinhart, T. R. / Spear, S. / Strabel, G. / Veeck, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 888
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Electron Beam Welding of F-22 StructuresZenas, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 891
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Effects of Dent Removal on the Design Properties of Fuselage Skin MaterialSimmons, F. / Veciana, J. A. / Wallace, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 902
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Analysis and Testing of Extension Twist Coupled Composites Using Symmetric ConfigurationsArmanios, E. / Gregory, R. O. / Schleisman, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 908
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Characteristic-Mode-Based Component Mode Synthesis for Power Flow Analysis of Complex StructuresCastanier, M. P. / Pierre, C. / Tan, Y.-C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 918
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Nonlinear Responses of Symmetrically Laminated Composite Cantilever BeamsArafat, H. N. / Nayfeh, A. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 929
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Predicting the Impact Response of an Energy-Absorbing Composite Subfloor BeamKellas, S. / Knight, N. F. / Pinson, L. D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 940
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Passively Damped Vibration of Composite Plates with Zig-Zag ElementsKosmatka, J. B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 951
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Impact Sound Realization of Composite StructuresHwang, J. S. / Kim, S. J. / Song, J. Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 960
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A Higher-Order Sandwich Plate Theory Accounting for 3-D StressesPai, P. F. / Palazotto, A. N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 971
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Composite Grid Structure with Near-Zero Thermally Induced DeflectionKim, C. K. / Lee, H. J. / Park, H. C. / Yoon, K. J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 977
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Nonlinear Analysis of the Cured Shape and Residual Stress of Unsymmetric Composite LaminatesCho, M. / Yoo, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 984
-
Innovative Deployable Antenna Developments Using Tensegrity DesignCrane, C. D. / Duffy, J. / Knight, B. F. / Rooney, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 995
-
A New Bonded Wavy Composite Lap JointSun, C. T. / Zeng, Q. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1004
-
Expedient Unsteady Transonic Solutions Above and Below Freestream Mach OneChen, P. C. / Liu, D. D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1015
-
Prediction of Aeroacoustic Noise Generated by Viscous Flow Around Rectangular Cross SectionsLee, J. / Yoo, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1025
-
Simply Implementing Non-Rational Function Gust Filters for Real Time Simulation ApplicationChristhilf, D. M. / Pototzky, A. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1034
-
Correction of Unsteady Aerodynamic Influence Coefficients Using Experimental or CFD DataBrink-Spalink, J. / Bruns, J. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1039
-
Enhanced Damping of Continuous Wave Fiber Composite Sandwich PanelsJensen, D. W. / Steurer, K. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1047
-
Unified Approach to Modeling Matrix Cracking in Laminated Composite StructuresChattopadhyay, A. / Thornburgh, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1055
-
Higher-Order Asymptotic Model for a Heterogeneous Beam, Including Corrections Due to End EffectsBuannic, N. / Cartraud, P. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1064
-
Nonlinear Bulging Factors for Longitudinal and Circumferential Cracks in Cylindrical Shells Subjected to Combined LoadsRose, C. A. / Starnes, J. H. / Young, R. D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1079
-
Influence of Geometric Nonlinearities on the Response and Failure of Internally Pressurized Elliptical Composite CylindersHyer, M. W. / McMurray, J. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1090
-
Crack Path Bifurcation at a Tear Strap in a Pressurized ShellCowan, A. L. / Davila, C. G. / Johnson, E. R. / Starnes, J. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1102
-
Structural Optimization for Light-Weight Articulated Rotor BladeKim, J.-E. / Sarigul-Klijn, N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1113
-
Optimization of Car Body under Constraints of Noise, Vibration, and Harness (NVH), and CrashKodiyalam, S. / Sobieski, J. / Yang, R.-J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1129
-
Optimization of Mistuned Bladed Discs Using Gradient-based Response Surface ApproximationsHaftka, R. T. / Petrov, E. P. / Vitali, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1140
-
Analysis and Optimization of Mid-Plane Asymmetric Sandwich Beams under Lateral Loading Including Buckling EffectsSatapathy, N. / Vinson, J. R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1148
-
Integrated Optimization of Viscoelastic Structures and Active Controllers for Flexible Space StructuresOnoda, J. / Uchida, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1159
-
Detection and Correction of Poorly Converged Optimizations by Iteratively Reweighted Least SquaresGrossman, B. / Haftka, R. / Kim, H. / Mason, W. / Papila, M. / Watson, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1177
-
Dynamic Taxi, Take-Off, and Landing Roll Analyses for Large Business Jet AircraftBrodman, H. / Freund, D. / Hanson, L. / McKissack, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1188
-
Finite Elements in Time Domain for Optimal Control Using Higher-Order Shape FunctionsKapania, R. K. / Kim, S. J. / Park, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1194
-
Modeling of Frequency Dependent Properties of Viscoelastic Materials Subjected to Shock LoadsInman, D. J. / Lesieutre, G. A. / Rusovici, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1205
-
Transient Response of Contacting Plates Subject to Close Proximity Blast LoadsCoggin, J. M. / Johnson, E. R. / Kapania, R. K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1215
-
On the Understanding of Snap-Through Phenomenon in Aerothermoelasticity of PanelsUdrescu, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1224
-
Investigation of Curved Composite Panels Under High-G LoadingJenkins, S. N. / Spearing, S. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1234
-
Stiffness Tailoring of Tension-Loaded Composite Panels to Contain DamageBhatia, N. / Ley, R. P. / Lin, W. / Mahler, M. A. / Patel, N. / Wolf, E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1243
-
Propagation and Control of Crack-Like Damage in Curved Composite Combined LoadsLey, R. P. / Lin, W. / Mahler, M. A. / Rouse, M. / Shah, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1252
-
The Reliability of Adhesive Joints Under Piezomechanical LoadingSanders, C. / Shaw, M. / Spearing, S. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1261
-
Predictor-Corrector Approach for the Analysis of Sandwich PanelsKim, Y. H. / Park, J. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1271
-
Fixed-Order Mixed Norm Designs for Building Vibration ControlCalise, A. J. / Hsu, C. C. / Whorton, M. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1280
-
Cargo-Pendulation Reduction in Boom Cranes Via Cable-Length ManipulationAbdel-Rahman, E. M. / Nayfeh, A. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1288
-
Nonlinear Control of a Parametrically Excited Structural Dynamic Model of an F-15 Tail SectionEl-Badawy, A. / Nayfeh, A. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1299
-
Cargo Pendulation Reduction on Ship-Mounted Cranes via Boom-Luff and Slew Angles ActuationHenry, R. J. / Masoud, Z. N. / Mook, D. T. / Nayfeh, A. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1305
-
Fracture Parameter Evaluation of Composite Panels Under In-Plane LoadingCai, G. X. / Yuan, F. G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1316
-
Prediction of Fretting Fatigue Crack Initiation Based on the Plane of Maximum Shear Stress AmplitudeJain, V. / Lykins, C. / Mall, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1326
-
Influence of Contact Profile on Fretting Crack Nucleation in a Titanium AlloyFarris, T. N. / Harish, G. / Murthy, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1334
-
Tests of Braided Composite Fuselage Frames under Radial Inward LoadBoitnott, R. L. / Johnson, E. R. / Perez, J. G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1344
-
Investigation of Impact Damage in aCFRP Wingbox under LoadClarke, A. / Greenhalgh, E. S. / Millson, B. / Thompson, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1355
-
On the Use of Energy Minimization for CA Based Analysis in ElasticityHajela, P. / Kim, B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1366
-
Genetic Algorithms for the Optimization of Piezoelectric Actuator LocationsKapania, R. / Sheng, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1377
-
Genetic Algorithm Approaches to Smart Actuator Placement for Aircraft Flight ControlCook, A. M. / Crossley, W. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1387
-
Using a Genetic Algorithm to Design Beam Cross-Sectional Topology for Bending, Torsion, and Combined LoadingCrossley, W. A. / Fanjoy, D. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1396
-
Genetic Algorithm Based Design of Transonic Airfoils Using Euler EquationsJang, M. / Lee, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1405
-
On the Simulation of Crack-Propagation in Pressurized ShellsRankin, C. C. / Riks, E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1416
-
Collapse of Elastic-Plastic Plates with CracksCorona, E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1421
-
Analysis and Test of Repair Concepts for a Carbon-Rod Reinforced LaminateBaker, D. J. / Rousseau, C. Q. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1431
-
Microstructure and Creep Behavior of Self-Reinforced Silicon Nitride Ceramics Heat-Treated by Furnace and Microwave AnnealingNarayan, J. / Sankar, J. / Wei, Q. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1439
-
Microstructure and Mechanical Evaluations of Sintered Si3N4Kelkar, A. / Russell, L. / Sankar, J. / Wei, Q. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1448
-
Mechanical Performance of CF/Polymer Composite Laminates under Cryogenic ConditionsAoki, T. / Ishikawa, T. / Kumazawa, H. / Morino, Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1456
-
"In-situ" Characterization of Thermal Degradation in Graphite/Polymeric CompositesLin, K. Y. / Ohno, S. / Ohuchi, F. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1465
-
A Closed-Form Expression for Strain Energy Release Rate of DelaminationChan, W. S. / Kuo, W. J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1473
-
A Novel Mode I Fracture Test for Stitched Composite LaminatesChen, L. / Ifju, P. G. / Sankar, B. V. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1481
-
DCB Test and Analysis of New 3-D Orthogonal Interlocked Fabric CompositeNishii, N. / Watanabe, N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1492
-
Analytical Solution for a Cracked Mosaic Model of Woven Fabric CompositesGao, X.-L. / Mall, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1503
-
Active Aeroelastic Tailoring with Adaptive Continuous Control SurfacesDobbins, A. / Duke, D. K. / Weisshaar, T. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1514
-
Nonlinear Aeroelastic Response of a Typical Airfoil Section with Control Surface FreeplayDowell, E. / Kholodar, D. / Tang, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1524
-
Aeroelastic Modeling of Trailing-edge Flaps with Smart Material ActuatorsChopra, I. / Shen, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1538
-
Aeroelastic Analysis of a Composite Wingbox with Varying Root FlexibilityBattoo, R. S. / De Baets, P. / Mavris, D. N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1547
-
Static Aeroelastic Stability of the Reversed Sweep Wing ConfigurationPopescu, B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1554
-
Comparison of Preliminary Designs of Stiffened Panels Optimized Using PANDA2 For Reusable Launch Vehicle Propellant TanksHaftka, R. T. / Lamberti, L. / Venkataraman, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1586
-
Effective Widths of Compression-Loaded Plates with a CutoutHilburger, M. W. / Nemeth, M. P. / Starnes, J. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1604
-
Optimum Design and Testing of a Post-Buckled Stiffened PanelButler, R. / Hunt, G. W. / Kennedy, D. / Lillico, M. / Watson, A. / Williams, F. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1614
-
Bending Boundary Layers in Laminated Composite Circular Cylindrical ShellsNemeth, M. P. / Smeltzer, S. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1646
-
Inclusion of Local Postbuckling Response in the Design of Stiffened PanelsAnderson, M. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1654
-
Optimal Design of Grid-Stiffened Panels and Shells with Variable CurvatureAmbur, D. R. / Jaunky, N. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1663
-
Automated Optimization of Shells of RevolutionBushnell, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1714
-
An Integrated Multidisciplinary Design Optimization Procedure for Cooled Gas Turbine BladesChattopadhyay, A. / Rajadas, J. N. / Talya, S. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1727
-
An Interactive Multiobjective Optimization Design Strategy for Multidisciplinary SystemsRenaud, J. E. / Rodriguez, J. F. / Tappeta, R. V. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1742
-
Physical Programming's Ability to Generate a Well-Distributed Set of Pareto PointsMessac, A. / Sundararaj, G. J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1755
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Manufacturability Based Optimization of Aircraft Structures Using Physical ProgrammingMartinez, M. / Messac, A. / Rais-Rohani, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1768
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Virtual Stability Prototyping of Doubly Curved Orthotropic Panels via Philips Optimisation StrategyArbocz, J. / Bouwman, V. P. / de Vries, J. / Stehouwer, P. / ter Weeme, B. J. W. / Zhang, G. Q. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1777
-
A Sensitivity Based Methodology for Multiobjective and Multidisciplinary OptimizationHernandez, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1787
-
High Quality Static Response Approximations Derived from the Sherman-Morrison IdentitySmaoui, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1798
-
Durability of a Woven Polymer Matrix Composite in Aerospace ApplicationsCase, S. W. / Patel, S. R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1809
-
Modeling of Hygrothermal and Aging Effects in Textile CompositesDharani, L. / Gupta, V. / Roy, S. / Xu, W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1820
-
Experimental Characterization of Hygrothermal and Aging Effects in Textile CompositesDharani, L. R. / Gupta, V. / Roy, S. / Xu, W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1829
-
Long-Term Durability of Polymer Matrix Composites Under Simulated Supersonic Flight Profile TestingGates, T. S. / Whitley, K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1841
-
Fatigue Damage Evolution in Woven Fabric CompositesKumar, R. / Talreja, R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1850
-
Vibration Reduction in Rotocraft Using an Enhanced ACSR ModelCribbs, R. / Friedmann, P. P. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1865
-
Aeroelastic Scaling for Fixed and Rotary-Wing Aircraft with ApplicationsFriedmann, P. P. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1880
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Helicopter Aeroelastic Response and Stability Using a Refined Time Domain Elastomeric Damper ModelBrackbill, C. R. / Lesieutre, G. A. / Smith, E. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1897
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Nonlinear Analysis of Helicopter Ground ResonanceKunz, D. L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1905
-
Influence of Nonlinear Elastomer on Isolated Lag Dynamics and Rotor/Fuselage Aeromechanical StabilityMallik, A. K. / Pohit, G. / Venkatesan, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1916
-
Analysis and Manufacture of Dynamically Scaled Wind Tunnel ModelAdrezin, R. / Gates, A. / Wei, J. / Yarlett, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1922
-
Fin Buffeting Features of an Early F-22 ModelHuttsell, L. / Moses, R. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1932
-
Practical Implementation of Non-Contacting Laser Strain Measurement SystemsKadambi, J. R. / Quinn, R. D. / Yunis, I. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1943
-
Experimental Steady and Unsteady Aerodynamic and Flutter Results for HSCT Semispan ModelsCole, S. / Florance, J. R. / Keller, D. F. / Scott, R. / Silva, W. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1954
-
Empirical Investigation of Structural Dynamics Under Zero-Gravity and Its Comparison to On-Ground MeasurementsHamacher, H. / Ory, H. / Stark, H. R. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1964
-
Experimental Damage Detection Using Substructural Transmission ZerosPark, K. C. / Reich, G. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1975
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An Experimental Investigation of Piezoelectric Coupling in Jet Engine Fan BladesGordon, R. W. / Hollkamp, J. J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1984
-
Prestack Reverse-time Migration in Structure Health MonitoringLin, X. / Yuan, F. G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 1995
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Torsional Buckling Analysis of Composite CylindersCho, C. / Choi, Y. / Park, H. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2003
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Buckling Analysis for Laminated Plates with Multiple DelaminationCho, M. / Kim, J.-S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2014
-
Postbuckling Analysis of Delaminated Composite Plates Using Zig-Zag Theory with Contact ConditionsBaranski, A. / Biggers, S. B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2021
-
Dynamic Stability Analysis of Doubly Curved Orthotropic Shells Under ImpactBouwman, V. / ter Weeme, J. W. / van Campen, D. H. / Zhang, J. / Zhang, K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2030
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Computational Simulation of Composite Fatigue LifeChamis, C. / Minnetyan, L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2040
-
Bearing/By-Pass Load Interaction Effects on Strength of CMC JointsForeman, C. / Nagar, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2048
-
A Micromechanics Based Predictive Model for Damage Initiation in Compressively Loaded Angle Ply Composite LaminatesAhn, J. / Waas, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2058
-
Corrosion Prediction in Aging Aircraft Materials using Neural NetworksBailey, R. A. / Jayanti, S. / Palakal, M. J. / Pidaparti, R. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2066
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Voxel-Based Unit Cell Homogenization of Textile CompositesKim, H. / Lakes, R. S. / Swan, C. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2073
-
Developments in the Homogenization of Elastic Properties for Complex Three-Dimensional Composite StructuresChung, P. W. / Somkanae, A. / Tamma, K. K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2084
-
Three Dimensional Finite Element Analysis of Twill Woven Composite LaminatesChaphalkar, P. / Kelkar, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2094
-
Analysis of Complex Nonlinear SystemsGrigoriu, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2102
-
Cut-Outs Subjected to Combined Mechanical, Thermal, and Acoustic LoadingEslami, H. / Gangadharan, S. N. / Ho, J. F. / Nagendra, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2113
-
Optimal Design of Non-Deterministic Systems Utilizing Min-Max FormulationAli, M. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2117
-
Methods for Robust Multidisciplinary DesignChen, W. / Du, X. / Wang, Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2127
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Topology Optimization for Structures Under Uncertain LoadsFuruya, H. / Igarashi, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2134
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Damage Tolerance of a Cylindrical Shell Containing a Crack Under Single and Combined LoadsArbocz, J. / Hoogkamer, D. / Waas, A. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2146
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Energy Absorption Capacity of Graphite-Epoxy Tubular SpecimensFuchs, H. / Hyer, M. W. / Schultz, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2157
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Transhab: NASA's Large-Scale Inflatable Spacecraftde la Fuente, H. / Raboin, J. / Spexarth, G. / Valle, G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2166
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Overcoming the Obstacles to Using a Genetic Algorithm for Topology Design of Planar Cross-SectionsCrossley, W. A. / Fanjoy, D. W. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2175
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Role of Automatic Differentiation in Concurrent Subspace Optimization MethodLee, J. / Park, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2185
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An Integrated Approach for Topology and Shape Optimizations of 3D Structural ComponentsChang, K.-H. / Tang, P.-S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2196
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Reduced Basis Representation of Large-Scale Random Eigenvalue ProblemsKeane, A. J. / Nair, P. B. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2207
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Microstructure-Based Stochastic Finite Element MethodsOstoja-Starzewski, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2214
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An On-Line Flutter Analysis SystemLo, W. / Shih, C. / Yan, C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
- 2222
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An Inflatable Microstrip Reflectarray Concept for KA-band ApplicationsCadogan, D. / Feria, V. / Huang, J. / Lin, J. K. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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On Budiansky's Problem in Nonlinear Stochastic BucklingElishakoff, I. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Cellular Automata for Design of Truss Structures with Linear and Nonlinear ResponseGurdal, Z. / Soremekun, G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Effect of Spar-Rib Orientation on Strain Energy in the Roll Maneuver of a Wing without AileronsKhot, N. S. / Veley, D. E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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PACKS: A Structural Definition Process for CompositesHale, R. D. / Miller, N. F. / Vasey-Glandon, V. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Designing Turbine Blade Internal Cooling Passages Using Response Surface and Kriging MethodologiesDonahoo, E. E. / Simpson, T. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Single and Multi-cell Composite Thin Walled BeamsHodges, D. / Volovoi, V. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Debonding of Stitched Composite Sandwich StructuresGlaessgen, E. H. / Raju, I. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Evaluation of Equivalent Laminated Plate Solution (ELAPS) in HSCT SizingBecker, B. T. / Bhatia, K. G. / Boyd, W. N. / Henderson, J. L. / Nazari, M. M. / Stone, S. C. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Flexible Multibody Dynamics Equations with Constant "Mass Matrix"Banerjee, A. K. / Chien, L. S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Active Control of Airframe Response with Distributed Smart ActuatorsChopra, I. / Park, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Modified Short Beam Shear Test for Measurement of Interlaminar Shear StrengthAbali, F. / Shivakumar, K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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"Dancing" Wind Tunnel Models for the Direct Measurement of Generalized Unsteady Aerodynamic LoadsLivne, E. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Plane Strain Radial Flow of Rigid/Hardening Solids - Part II: Effects of Material Non HomogeneityDurban, D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Crack Tip Fields in Anisotropic ShellsYang, S. / Yuan, F. G. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Evaluation of Fracture Modes in Mixed Mode Delamination ProblemsArmanios, E. / Makeev, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Conservative Interpretation of Aerodynamic Loads for Aeroelastic CompuationsHabashi, W. G. / Lepage, C. Y. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Simulation of Delamination Buckling and Growth in Composite StructuresNilsson, K.-F. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Prebuckling and Postbuckling Response of Tailored Composite Stiffened Panels with Axial-Shear CouplingHyer, M. W. / Starnes, J. H. / Young, R. D. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Influence of Target and Impactor Parameters on the Nonlinear Response and Residual Strength of Curved Thin Composite PlatesAmbur, D. / Starnes, J. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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The Development and Application of Titanium 6 Al-4V ELI Beta Annealed Investment Castings to Fracture Critical Structure of the F-22 Air Dominance FighterLane, J. / Smith, P. / Gallager, M. / Travinski, D. / Phelps, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Titanium Alloy Sructures for Air Frame Application by Laser Forming ProcessArcella, F. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Method for Evaluating the Deployment Characteristics of a Modular-type ReflectorAndo, K. / Ishikawa, H. / Watanabe, M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Effects of CPC's and Clamping Force on Fatigue Behaviour of Bolted JointsDhamari, R. / Shankar, K. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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An Advanced Buffet Load Alleviation SystemHopkins, M. A. / Pitt, D. M. / White, E. V. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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A Complex Velocity Solution fo the Flutter EquationsPitt, D. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Evaluation of Alpha Case on Titanium Casting SpecimensPhelps, H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Aluminum Alloys for the Transport Industry: Environmental Degradation and Microstructure RelationshipAlvarez, A. / Froes, F. H. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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An Evaluation of Mixed-Mode Energy-Release Rates in the Cracked Sandwich Beam SpecimenShivakumar, K. N. / Smith, S. A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Size Scales for Accurate Homogenization in the Presence of Severe Stress GradientsPagano, N. / Yuan, F. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Failure of Laminated Composites at Thickness Discontinuities under Complex Loading and Elevated TemperaturesKnauss, W. / Lee, S. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Multi-body Dynamics Metamodels for System Level Studies of New Tilt-Rotor TechnologiesBaker, A. / Bauchau, O. / Mavris, D. / Volovoi, V. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Theory of Anisotropic Beams with Hygrothermal Effects and Integral ActuatorsBadir, A. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000
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Damage Progression in Buckle-Resistant Notched Composite Plates Loaded in Uniaxial CompressionAmbur, D. R. / Davila, C. G. / McGowan, D. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers / American Society of Civil Engineers et al. | 2000