Adaptive Control for Interior Noise Control in Rocket Fairings (English)
- New search for: McEver, M.
- New search for: Moon, S.
- New search for: Clark, R.
- New search for: Cole, D.
- New search for: American Institute of Aeronautics and Astronautics
- New search for: McEver, M.
- New search for: Moon, S.
- New search for: Clark, R.
- New search for: Cole, D.
- New search for: American Institute of Aeronautics and Astronautics
In:
Structures, structural dynamics, and materials conference
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3781-3790
;
2003
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ISBN:
- Conference paper / Print
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Title:Adaptive Control for Interior Noise Control in Rocket Fairings
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Contributors:McEver, M. ( author ) / Moon, S. ( author ) / Clark, R. ( author ) / Cole, D. ( author ) / American Institute of Aeronautics and Astronautics
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Conference:44th, Structures, structural dynamics, and materials conference ; 2003 ; Norfolk, VA
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Published in:PAPERS- AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS ; 5 ; 3781-3790
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Publisher:
- New search for: AIAA
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Publication date:2003-01-01
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Size:10 pages
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Remarks:Contains papers also from: 11th AIAA/ASME/AHS adaptive structures conference, 5th AIAA non-deterministic approaches forum, 4th AIAA gossamer spacecraft forum, and AIAA dynamics specialists conference. Contains papers AIAA-2003-1401 to AIAA-2003-2008 only with gaps
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ISBN:
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Type of media:Conference paper
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Type of material:Print
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Language:English
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Keywords:
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Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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A Quasi-linear Approach for Solving Aeroelastic Problems Involving Aerodynamic and Structural NonlinearitiesMunteanu, S. / Rajadas, J. / Nam, C. / Chattopadhyay, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2
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Critical Issues in the UNIDROIT Draft Space ProtocolLarsen, P. / International Astronautical Federation et al. | 2003
- 12
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The Concepts of Assets and Property: Similarities and Differences, and their Applicability to Undertakings in Outer SpaceOspina, S. / International Astronautical Federation et al. | 2003
- 12
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Modeling Aerodynamic Nonlinearities for Two Aeroelastic Configurations: Delta Wing and Flapping FlagAttar, P. / Dowell, E. / Tang, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 23
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Time Simulations of the Response of Maneuvering Flexible AircraftMeirovitch, L. / Tuzcu, I. / American Institute of Aeronautics and Astronautics et al. | 2003
- 23
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Developing Countries and the UNIDROIT Protocol on Space Propertydos Santos, A. F. / International Astronautical Federation et al. | 2003
- 33
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Evolution of Space Law in France Main Lines of the 2002 Study Report for the MinisterClerc, P. / International Astronautical Federation et al. | 2003
- 38
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Unsteady Sonic Aerodynamics Using Acceleration Potential ApproachChen, P. / Liu, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 44
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Space DebrisLafferranderie, G. / International Astronautical Federation et al. | 2003
- 47
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Accurate Flutterometer Predictions Using Volterra Modeling with Modal Parameter EstimationLind, R. / Mortagua, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 51
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Challenges to Space Law in the 21st Century - Project 2001 PlusHobe, S. / Hettling, J. K. / International Astronautical Federation et al. | 2003
- 56
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Privateering and Profiteering on the Moon and Other Celestial Bodies: Debunking the Myth of Property Rights in SpaceSterns, P. M. / Tennen, L. I. / International Astronautical Federation et al. | 2003
- 56
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Estimating Nonlinearity Using Volterra Kernels in Feedback with Linear ModelsLind, R. / Prazenica, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 67
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Identification of CFD-Based Unsteady Aerodynamic Models for Aeroelastic AnalysisRaveh, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 70
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Implementation of Intellectual Property Law on the International Space StationMannix, J. G. / International Astronautical Federation et al. | 2003
- 77
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Application of the Rules of the Code of Conduct to the First Crews on Board the International Space StationSgrosso, G. C. / International Astronautical Federation et al. | 2003
- 79
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Application of Ho's Algorithm to Identify an Aeroelastic System by a Linear State-Space ModelRodrigues, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 84
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Status of Multilateral Space Agreements in International and United States LawGantt, J. B. / International Astronautical Federation et al. | 2003
- 98
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Commitment and Compliance in the Evolution of the ISS ProgramCovert, L. / International Astronautical Federation et al. | 2003
- 100
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The Unscented and Extended Kalman Filter for Systems with Polynomial Restoring ForcesPopescu, C. / Wong, Y. / American Institute of Aeronautics and Astronautics et al. | 2003
- 111
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Hybrid Frequency-Time Domain Methods for the Analysis of Complex Structural Systems with Dry Friction DampingPierre, C. / Poudou, O. / American Institute of Aeronautics and Astronautics et al. | 2003
- 112
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Legal Aspects of Space TourismJakhu, R. / Bhattacharya, R. / International Astronautical Federation et al. | 2003
- 125
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Transonic/Supersonic Aeroelastic Instability of an All Movable Wing with Structural NonlinearityKim, D. / Lee, I. / Kim, T. / Lee, J. / Moon, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 134
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International Agreements of Unlimited Duration: The 1972 ABM TreatyChristol, C. Q. / International Astronautical Federation et al. | 2003
- 139
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The Jus ad Bellum in Outer Space: The Interrelation Between Article 103 of the Charter of the United Nations and Article IV of the Outer Space TreatyLee, R. J. / International Astronautical Federation et al. | 2003
- 139
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Experimental Investigation of an All-Movable Vertical Tail ModelCooper, J. / Sensburg, O. / Amprikidis, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 149
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Missile Defense and International LawHashimoto, Y. / International Astronautical Federation et al. | 2003
- 150
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Active Aeroelastic Control of 2-D Wing-Flap Systems in an Incompressible FlowfieldLibrescu, L. / Na, S. / Marzocca, P. / Chung, C. / Kwak, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 153
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The Doctrine "Rebus Sic Stantibus" and the 1972 ABM Treaty: A Brief ReflectionAndem, M. N. / International Astronautical Federation et al. | 2003
- 161
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Control Law Design in a Computational Aeroelasticity EnvironmentNewsom, J. / Robertshaw, H. / Kapania, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 162
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Military Space Activity in the Light of General International LawGal, G. / International Astronautical Federation et al. | 2003
- 171
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Elendilmir: Satellites-Threats or the Threatened?Goh, G. M. / International Astronautical Federation et al. | 2003
- 174
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Divergence Experiment Prediction Techniques of Flat-Plate Forward-Swept Wing in Wind TunnelWan, Z. / Yang, C. / Zou, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 180
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The Optimisation of Foam-filled Cylindrical Shells Subject to Flexural LoadingCecchini, L. / Weaver, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 186
-
Cooperation v. Control: Military Strategy Challenging LawDriscoll, C. M. / International Astronautical Federation et al. | 2003
- 188
-
Theory of Initially Twisted, Composite, Thin-walled BeamsHodges, D. / Yu, W. / Volovoi, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 195
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The Timoshenko-like Theory of the Variational Asymptotic Beam Sectional AnalysisHodges, D. / Yu, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 197
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Legal and Political Implications of Offensives Actions From and Against the Space SegmentDe Angelis, I. M. / International Astronautical Federation et al. | 2003
- 205
-
Optimization of Elastically Tailored Tow-Placed Plates with HolesTatting, B. / Gurdal, Z. / Jegley, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 206
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The Vanishing Horizon: Will the Asymmetric Battlefield Make Space-Based Weapons a Reality?Heath, J. W. / International Astronautical Federation et al. | 2003
- 216
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Militarization of Spacede Cocca, M. M. E. / International Astronautical Federation et al. | 2003
- 219
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On Superior Buckling Performance of Flat Plates Through AnisotropyWeaver, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 227
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Operational Capabilities and Legal Implications of a Military Space PlaneCharania, A. C. / International Astronautical Federation et al. | 2003
- 230
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Behavior of Non-Circular Sandwich Cylindrical Shells Subject to Internal PressurizationPreissner, E. / Vinson, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 236
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Prevention of the Outer Space WeaponizationZhukov, G. P. / International Astronautical Federation et al. | 2003
- 241
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Structural Stability of a Stiffened Aluminum Fuselage Panel Subjected to Combined Mechanical And Internal PressureRouse, M. / Young, R. / Gehrki, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 248
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GNSS for Military Uses or Peaceful Uses?Takaya, Y. / International Astronautical Federation et al. | 2003
- 251
-
An Analysis of the F/A-18C/D Limit Cycle Oscillation SolutionYurkovich, R. / Goodman, C. / Reichenbach, E. / Hood, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 257
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In-Flight Wing Deformation Characteristics During Limit Cycle OscillationsDenegri, C. / Dubben, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 258
-
Propaganda via SatelliteAchilleas, P. / International Astronautical Federation et al. | 2003
- 263
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Acquisition of Space Weapons, the Legal, Political and Military Impact for International Peace and SecurityCatena, J. / International Astronautical Federation et al. | 2003
- 267
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Limit Cycle Oscillation Flight Test Results for Asymmetric Store ConfigurationsDawson, K. / Maxwell, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 278
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Impact of Frictional Structural Nonlinearity in the Presence of Negative Aerodynamic DampingMignolet, M. / Agelastos, A. / Liu, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 280
-
Perceptions on the Definition of a "Launching State" and Space Debris RisksWilliams, M. / International Astronautical Federation et al. | 2003
- 286
-
A New Look at the "Launching State" - the Results of the UNCOPUOS Legal Subcommittee Working Group 2000-2002Schrogl, K.-U. / Davies, C. / International Astronautical Federation et al. | 2003
- 289
-
Modeling Limit Cycle Oscillations for an NLR 7301 Airfoil Aeroelastic Configuration Including Correlation with ExperimentThomas, J. / Dowell, E. / Hall, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 298
-
Progressive Failure Analysis of RLV Laminates of IM7/PETI-5 at High, Room, and Cryogenic TemperaturesSu, X. / Abdi, F. / American Institute of Aeronautics and Astronautics et al. | 2003
- 302
-
Brazil-Ukraine Partnership for the Use of the Alcantara Launch CenterLeister, V. / Filho, J. M. / International Astronautical Federation et al. | 2003
- 310
-
Launching Alcantara into the Global Space Economy-The 2001 Brazilian National Space Lawvon der Dunk, F. G. / International Astronautical Federation et al. | 2003
- 311
-
Mode I Fracture of Polymer Matrix Composites to -269^oCDonaldson, S. / Kim, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 315
-
Mechanical Characterization and Ultrasonic NDE of Cryogenic CompositesKinra, V. / Lagoudas, D. / Whitcomb, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 321
-
The Impact of Arms Limitation Agreements and Export Control Regulations on Launch ActivitiesFreeland, S. R. / Lee, R. J. / International Astronautical Federation et al. | 2003
- 323
-
Evaluation of Cryogenic Shear Performance of CFRP LaminatesHe, J. / Morino, Y. / American Institute of Aeronautics and Astronautics et al. | 2003
- 331
-
Licensing Procedure Established in the Mexican Law for the Operation of Satellite Orbits Assigned to Mexico and for the Transmission of Signals Coming from Foreign Satellitesde Arellano, R. M. R. / Arvide, Y. / International Astronautical Federation et al. | 2003
- 332
-
Evaluation of Electrically Disbonding Adhesive Properties for use as Separation SystemsWelsh, J. / Higgins, J. / Gilbert, M. / Cogan, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 339
-
The Brazilian Space Licensing Regulationda Veiga, A. S. / International Astronautical Federation et al. | 2003
- 342
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Luminescent Strain Sensitive CoatingsHubner, J. / Ifju, P. / Schanze, K. / Jaing, S. / Liu, Y. / El-Ratal, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 346
-
Evolving Space Law and World Political HegemoniesFilho, J. M. / Salin, P. A. / International Astronautical Federation et al. | 2003
- 352
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Consideration of Ionic Polymer Materials as Flapping Mechanisms for Micro-Air VehiclesAkle, B. / Leo, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 356
-
U.S. Export Controls and Litigation of Contracts: Another Example of the Law of Unintended ConsequencesSchwetje, F. K. / Burnett, D. J. / International Astronautical Federation et al. | 2003
- 362
-
A Domain Evolution Model for the Ferroelectric Hysteresis of Piezoceramic MaterialsLu, X. / Hanagud, S. / Narayanan, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 364
-
Learning from the X-Prize ExperienceWalker, C. H. / International Astronautical Federation et al. | 2003
- 370
-
Arresting Cracks in Bone-like CompositesHuang, J. / Rapoff, A. / Haftka, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 375
-
The Lunar Base: Liability in PerspectiveWeidaw, K. M. / International Astronautical Federation et al. | 2003
- 381
-
Hydration and Control Assessment of Ionic Polymer ActuatorsKothera, C. / Leo, D. / Robertson, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 391
-
Multicriteria Decision Making for Production System Conceptual Design Using s-Pareto FrontiersMessac, A. / Maria, A. / Mattson, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 396
-
Satellite Technology as a Source of Integration. A Comparative Analysis: Europe/MERCOSURArganaras, L. F. C. / International Astronautical Federation et al. | 2003
- 401
-
Space Debris Measurement, Analysis and Study: A Tool for Global CooperationsBahrami, M. / Golrounia, A. / Moghani, T. / Shajiee, S. / International Astronautical Federation et al. | 2003
- 401
-
Bell-Curved Based Optimization for Mixed Continuous and Discrete Structural Optimization ProblemsKincaid, R. / Sobieszczanski-Sobieski, J. / Sykes, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 408
-
World Space Congress: "Legal and Policy Factors"Thorin, T. / International Astronautical Federation et al. | 2003
- 414
-
Mixed Discrete Synthetic Approach for Nonlinear Design OptimizationRao, S. / Xiong, Y. / American Institute of Aeronautics and Astronautics et al. | 2003
- 420
-
Need for Combining Space Law with Environmental Law and Global FederalismBhatt, S. / International Astronautical Federation et al. | 2003
- 422
-
Nonlinear Topology Design of Trusses Using Cellular AutomataGurdal, Z. / Missoum, S. / Abdalla, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 429
-
New Decision Matrix Based Approach for Concept Selection Using Linear Physical ProgrammingMessac, A. / Mullur, A. / Mattson, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 440
-
Rapid Structural Assessment Approach for Square Solar Sails Including Edge Support CordsMikulas, M. / Adler, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 454
-
Space Structures on the Back of an Envelope: John Hedgepeth's Approach to DesignLake, M. / Peterson, L. / Mikulas, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 468
-
Incongruent Interfaces in Three-Dimensional Finite Element ModelsMacNeal, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 480
-
Closed-Loop Deployable StructuresPellegrino, S. / Gan, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 489
-
Microdynamic Design Requirements for Large Space StructuresPeterson, L. / Hinkle, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 500
-
Structural Qualification of a Spacecraft Payload Using Near-Resonance Sine Burst TestingBarnes, D. / Pontius, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 508
-
Methods of Analyzing Surface Accuracy of Large Antenna Structures due to Manufacturing TolerancesMobrem, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 518
-
Optimization Strategies for the F/A-22 Horizontal StabilatorEngelstad, S. / Ellsworth, C. / Barker, D. / Proctor, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 529
-
Monolithic Structure: Materials and Methods for Reduced Cost, Reduced Weight and Improved Damage Tolerancevan der Veen, S. / Muzzolini, R. / Ehrstrom, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 539
-
SensorCraft Structural Optimization and Analytical CertificationRoberts, R. / Canfield, R. / Blair, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 549
-
Structurally Integrated Antennas on a Joined-Wing AircraftSmallwood, B. / Canfield, R. / Terzuoli, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 557
-
Use of Multibody Dynamics and Experimental In-flight Data for Load Analysis and Design Optimisation of Aircraft ComponentsVecchio, A. / Scionti, M. / Olbrechts, T. / De Voghel, R. / Van der Auweraer, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 568
-
Analysis and Test of Tailored Extension-Shear-Coupled Composite PanelsBaker, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 584
-
Nonlinear Modelling of Delaminated StrutsHunt, G. / Hu, B. / Butler, R. / Almond, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 591
-
Static and Dynamic Mechanical Influence of Fiber Waviness in Textile CompositesVilla, M. / Hale, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 600
-
Analysis of the Effects of Residual Strains and Defects on Skin/Stiffener Debonding Using Decohesion ElementsDavila, C. / Camanho, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 609
-
Elasticity Analysis and Optimization of a Functionally Graded Plate with HoleVenkataraman, S. / Sankar, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 622
-
Dynamic Analysis of Cross-ply Composite Laminates with Embedded Multiple DelaminationKim, H. / Chattopadhyay, A. / Ghoshal, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 633
-
Putting the Joint in Aircraft SurvivabilityWeisenbach, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 641
-
Vulnerability Assessment for DesignManion, J. / Dexter, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 648
-
Survivability Modeling and Validation in Complex Rib-Skin StructuresBurkhardt, J. / Joyce, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 656
-
Modeling the Anti-Helicopter Mine ThreatTownsend, S. / Olree, K. / Hayes, F. / Wright, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 663
-
High Strain Rate Response of Woven Graphite/Epoxy Composites at Elevated TemperaturesHosur, M. / Adya, M. / Dutta, P. / Jeelani, S. / Vaidya, U. / American Institute of Aeronautics and Astronautics et al. | 2003
- 674
-
Performance Evaluation and Modeling of Braided CompositesKelkar, A. / Tate, J. / Whitcomb, J. / Tang, X. / American Institute of Aeronautics and Astronautics et al. | 2003
- 685
-
A Material Model for Multi-Scale Analysis of Textile CompositesBahei-El-Din, Y. / Rajendran, A. / Zikry, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 691
-
Kinematics and Stiffness of Thermoformed Plain-Weave LaminatesHofstee, J. / van Keulen, F. / American Institute of Aeronautics and Astronautics et al. | 2003
- 702
-
Experimental Study on Z-pin Bridging Law by Pull-out TestsYan, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 707
-
Prediction of the Delamination Behaviour of Z-Fiber® Reinforced LaminatesCartie, D. / Partridge, I. / American Institute of Aeronautics and Astronautics et al. | 2003
- 713
-
Non-Deterministic Dynamic Instability of Composite ShellsChamis, C. / Abumeri, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 724
-
Application of Probabilistic Analysis to Aircraft Impact DynamicsLyle, K. / Padula, S. / Stockwell, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 735
-
Reliability Analysis with Adaptive Response SurfacesMahadevan, S. / Mourelatos, Z. / Zou, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 746
-
Creep Life Uncertainty Assessment of a Gas Turbine AirfoilWallace, J. / Wang, R. / Mavris, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 755
-
A Probabilistic Analysis to Quantify the Uncertainty in the Collapse Loading of Spherical Marine FloatsPepin, J. / Thacker, B. / Riha, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 769
-
Nonlinear Aeroelastic Analysis of Joined-Wing AircraftPatil, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 776
-
Analyses and Experiments of Suppression of Control Reversal Using a Wing Section with Multiple Control SurfacesPlatanitis, G. / Strganac, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 788
-
Flutter and Divergence Analysis Using the Generalized Aeroelastic Analysis MethodEdwards, J. / Wieseman, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 803
-
Design Studies of Aeroelastic Tailoring of Forward-Swept Composite Aircraft Using Hybrid Genetic AlgorithmWan, Z. / Yang, C. / Zou, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 813
-
Aeroelastic and Flutter Analysis of a Flexible WingLahidjani, M. S. / Ovesy, H. / Shams, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 825
-
An Improved Neural Network Model for Nonlinear Aeroelastic AnalysisVoitcu, O. / Wong, Y. / American Institute of Aeronautics and Astronautics et al. | 2003
- 836
-
Design of a Membrane Aperature Deployable StructureSmith, R. / Robertson, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 847
-
Deployment Accuracy and Mechanics of Elastic Memory CompositesMaji, A. / Campbell, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 857
-
Development and Testing of a Hinge/Actuator Using Elastic Memory CompositesFrancis, W. / Lake, M. / Mallick, K. / Freebury, G. / Maji, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 872
-
A High Precision Surface Shape Design for Large Deployable Mesh AntennaHarada, S. / Meguro, A. / Watanabe, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 879
-
Analytical and Experimental Frequency Verification of Deployed Satellite AntennasMisawa, M. / Ogawa, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 886
-
A Study into the Dynamics of Three Dimensional Tape Spring FoldsWalker, S. / Aglietti, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 894
-
A Guided Tradeoff for Cost and Weight for Generating Optimal Conceptual DesignsKelly, D. / Wang, K. / Dutton, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 905
-
Tradeoffs of Weight and Inspection Cost in Fail-safe DesignKale, A. / Haftka, R. / Papila, M. / Sankar, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 919
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Optimal Design and Damage Tolerance Verification of an Isogrid Structure for Helicopter ApplicationBaker, D. / Ambur, D. / Fudge, J. / Kassapoglou, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 938
-
Monte Carlo Simulation in Reliability Based Optimization Applied to Multidisciplinary System DesignBatill, S. / Padmanabhan, D. / Tappeta, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 949
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A Conceptual Design and Cost Optimisation MethodologyRaju, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 958
-
Study of Hygrothermal Isotropic Layup and Hygrothermal Curvature-Stable Coupling Composite LaminatesChen, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 968
-
Characterization of Polyimide Foams for Ultra-Lightweight Space StructuresVeazie, D. / Vincent, S. / Weiser, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 971
-
Through-the-Thickness Compression (ITTC) Properties for Laminated Composites - An Experimental StudyZhao, Y. / Thomas, F. / Kostreva, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 979
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Compressive Behavior of Hybrid CompositesWaas, A. / Yerramalli, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 988
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Single Fiber Fragmentation Test. A BEM AnalysisParis, F. / Varna, J. / Graciani, E. / Mantic, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 998
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Durability Characterization of Active Fiber Composite Actuators for Helicopter Rotor Blade ApplicationsWickramasinghe, V. / Hagood, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1008
-
Extension of the g-Method Flutter Solution to Aeroservoelastic Stability AnalysisKarpel, M. / Moulin, B. / Chen, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1014
-
Suppression of Supersonic Panel Flutter and Thermal Deflection Using Shape Memory AlloyGuo, X. / Mei, C. / Duan, B. / Abdel-Motagaly, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1024
-
Active Control of Nonlinear Panel Flutter Under Yawed Supersonic FlowMei, C. / Abdel-Motagaly, K. / Duan, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1040
-
Flutter Characterization of the Flexible HSCT Semispan ModelHajj, M. / Silva, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1049
-
Nonlinear Flutter of Curved Panels Under Yawed Supersonic Flow Using Finite ElementsAzzouz, M. / Przekop, A. / Guo, X. / Mei, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1060
-
Finite Element Modal Formulation for Hypersonic Panel Flutter Analysis with Thermal EffectsCheng, G. / Mei, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1071
-
Analysis of Helicopter Cabin Vibrations due to Rotor Asymmetry and Gust EncounterCoppotelli, G. / Mastroddi, F. / Gennaretti, M. / Cernicchiaro, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1081
-
Control Authority and the Design of Active Controllers for Buffet SuppressionPatel, U. / Roberts, P. / Henderson, D. / Hanagud, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1092
-
Theoretical/Experimental Study of Gust Alleviation Using an Electro-Magnetic Dry Friction DamperDowell, E. / Tang, D. / Gavin, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1109
-
Effect of Dissimilar Mating Materials on Fretting Fatigue of Ti-6Al-4VMall, S. / Lee, H. / Jin, O. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1117
-
Delamination Fracture Mechanics of Brittle and Toughened Composites Under the Influence of Mode III Stress-StateChen, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1129
-
A Model for Predicting the Overload Effects on Fatigue Crack Growth BehaviorManjunatha, C. / Parida, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1139
-
Application of Low Plasticity Burnishing to Improve Damage Tolerance of a Ti-6Al-4V First Stage Fan BladesPrevey, P. / Ravindranath, R. / Hornbach, D. / Cammett, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1148
-
Elevated Temperature Fretting of Turbine Materials Subjected to Engine Type-LoadingMurthy, H. / Farris, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1159
-
Optimal Overload Ratio Age Dependency in Fatigue Crack GrowthYu, S. / Newman, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1170
-
Behavior of Nitrided 32CrMoV13 Steel Subjected to Dent Initiated Rolling Contact FatigueJacq, C. / Nelias, D. / Lormand, G. / Vincent, A. / Dudragne, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1179
-
High Performance Computing and Rapid Visualization for Design Steering in MDOKodiyalam, S. / Yang, R. / Gu, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1187
-
WFC3 Optical Bench Structural Thermal Optical Performance (STOP) Analysis and OptimizationKunt, C. / Mule, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1196
-
Optimization of a Functionally Graded Metallic Foam Insulation Under Transient Heat Transfer ConditionsZhu, H. / Venkataraman, S. / Sankar, B. / Haftka, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1207
-
Fast Time Domain Simulation for Large-Order Linear Time-Invariant SystemsSou, K. / de Weck, O. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1221
-
Load Perturbation Design Approach for Repeatable Precision Deployable StructuresHeald, J. / Peterson, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1233
-
Computational Materials: Modeling and Simulation of Nanostructured Materials and SystemsGates, T. / Hinkley, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1247
-
Modeling of the Elastic Behavior of Double-Walled Carbon NanotubesChou, T. / Li, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1252
-
Calculation of Non-bonded Forces due to Sliding of Bundled Carbon NanotubesFrankland, S. / Bandorawalla, T. / Gates, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1263
-
The Effective Continuum Properties of Carbon and Inorganic NanotubesHeyliger, P. / Rappe , A. / Rousom, I. / Ramirez, F. / Tran, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1273
-
Carbon-Nanotube-Reinforced Structural Materials and Nonequilibrium Thermodynamic ModelsLu, X. / Hanagud, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1284
-
Experiment Design to Quantify Material MicroyieldDomber, J. / Hinkle, J. / Peterson, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1296
-
Optimal Control of Pretwisted Shearable Smart Composite Rotor BladesChandiramani, N. / Shete, C. / Librescu, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1307
-
Thin-Walled Rotating Blades made of Functionally Graded Materials: Modeling and Vibration AnalysisLibrescu, L. / Oh, S. / Song, O. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1318
-
Effect of Unsteady Blade Motion on the Aerodynamic Performance of Micro-RotorcraftKoratkar, N. / Kim, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1329
-
Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge FlapsSmith, E. / Wang, K. / Kim, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1341
-
Correlation of Tuned Free Vibration Characteristics with Mistuning Sensitivity for a Bladed DiskHussein, M. / Pierre, C. / Castanier, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1359
-
A Compact, Generalized Component Mode Mistuning Representation for Modeling Bladed Disk VibrationCastanier, M. / Pierre, C. / Lim, S. / Bladh, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1381
-
Imparting Desired Attributes by Optimization in Structural DesignSobieszczanski-Sobieski, J. / Venter, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1394
-
Road Response OptimizationChou, D. / Johnson, E. / Nack, W. / Schwerzler, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1405
-
Optimization Design of Composite Plates with Holes for Increased StrengthHuang, J. / Rapoff, A. / Haftka, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1416
-
SURVICE RT? Open Raytracing StandardButkiewicz, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1421
-
Meteoroid/Orbital Debris Risk Assessment for Resuseable Launch Vehicles Using Metallic TPSWilliamsen, J. / Bohl, W. / Galbraith, J. / Blosser, M. / Ahmed, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1430
-
Pultruded Composite Ballistic MaterialsHartman, P. / Erb, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1439
-
Testing of Torsional SMA Actuator in a Rotating Environment for a Variable Twist Tilt Rotor BladeAtulasimha, J. / Chopra, I. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1451
-
Smart Structures for Control of Optical SurfacesSobers, M. / Agnes, G. / Mollenhauer, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1462
-
Structural Tuning Through Embedded Angular MomentumPeck, M. / Cavender, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1470
-
Shape Adaptive Airfoils for Turbomachinery Applications Undergoing Large DeformationsMueller, T. / Lawerenz, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1480
-
Smart Armours made from Shape Memory MaterialsKamel, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1486
-
Automated Structural Integrity Monitoring Based on Broadband Lamb Wave Excitation and Matched FilteringKehlenbach, M. / Hanselka, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1493
-
A Multi-functional Stiffness/Energy Sensor for Damage PrognosticsWakha, K. / Majeed, M. / Pines, D. / Dasgupta, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1504
-
Damage Interrogation Using a Phased Piezoelectric Sensor/Actuator Array: Simulation Results on Two Dimensional Isotropic StructuresPurekar, A. / Pines, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1513
-
Computational Damage Tracking of Degrading Adaptive Composite StructuresMinnetyan, L. / Zhao, W. / Chamis, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1523
-
Delamination Effect on Transient History of Smart Composite PlatesGhoshal, A. / Chattopadhyay, A. / Kim, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1533
-
Multifunctional Vehicle Structural Health Monitoring Opportunities with Piezoelectric Wafer Active SensorsGiurgiutiu, V. / Barnes, J. / Thomas, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1544
-
Optimization Based Efficiencies in First Order Reliability AnalysisPeck, J. / Mahadevan, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1548
-
Expert Judgement and Bayesian Analysis of Turbine Rotor HCF ReliabilityBrown, J. / Pettit, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1558
-
A Strategy for Improving "Confidence" in a Failure ProbabilityAnnis, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1567
-
A Hybrid Possibilistic-Probabilistic Analysis Framework for Uncertainty ManagementWu, J. / Shin, Y. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1578
-
Variable Screening and Ranking Using Several Sampling Based Sensitivity MeasuresWu, J. / Mohanty, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1586
-
Aerodynamic Forces Approximation for Aeroservoelastic ModelsBotez, R. / Ibrir, S. / Biskri, D. / Hamza, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1595
-
Shape Optimization for Conforming AirfoilsRenaud, J. / Gano, S. / Batill, S. / Tovar, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1605
-
Aero-Structural Coupling and Sensitivity of a Joined-Wing SensorCraftSchwartz, J. / Canfield, R. / Blair, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1613
-
Design and Experimental Production of Small Deployable Mesh Type Reflector AntennaNagaoka, N. / Iikura, S. / Yamaguchi, I. / Kasai, T. / Igawa, H. / Nakajima, A. / Tsukumo, Y. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1622
-
Development of a Shockless Thermally Actuated Release Nut Using Elastic Memory Composite MaterialGall, K. / Lake, M. / Harvey, J. / Ricca, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1633
-
Sensitivity of Optimized Structures to Constraints and Performance Requirements for the SensorCraft ISR PlatformHenderson, J. / Martin, C. / Kudva, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1641
-
A Robust Algorithm for the Automated Design of Steel StructuresWilkerson, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1649
-
A Comparison of Recovery Methods for Reduced Dynamic Substructure Models with Internal LoadsFransen, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1660
-
Mathematical Modeling of Tailored Composite Tethers with Progressive Failure Using an Approximation TechniqueHa, K. / Dancila, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1671
-
Force Identification in a FGM Plate Using Truncated ResponseGopalakrishnan, S. / Chakraborty, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1680
-
Shock Response of a Damped Linear Structure Using GHM Finite ElementsMcTavish, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1689
-
Dynamic Response of a Flexible Structure Under Jet Plume Loading in a Planar OrbitMalla, R. / Lin, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1701
-
Damage Initiation and Progression in Internally Pressurized Noncircular Composite CylindersHyer, M. / Wolford, G. / Knight, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1712
-
Design with Explicit Safety Constraints and the Role of High-Fidelity AnalysesBackman, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1721
-
Damage Assessment for Composite Sandwich StructureWalker, T. / Graesser, D. / Ward, S. / Floyd, J. / Razi, H. / Ploubis, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1745
-
Computational Model for Progressive Failure of Adhesively Bonded JointsJohnson, E. / Goyal, V. / Cassino, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1760
-
Computational Modeling of Progressive Damage in Composite LaminatesWaas, A. / Basu, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1771
-
An Explicit Computational Formulation for Frictional Contact/Impact ProblemsTamma, K. / Zhou, X. / Sha, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1782
-
Thermal/Mechanical Durability of Polymer-Matrix Composites in Cryogenic EnvironmentsGates, T. / Whitley, K. / Grenoble, R. / Bandorawalla, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1794
-
Prediction of Delamination Growth and Opening near Intersection of Transverse Matrix Cracks and DelaminationWhitcomb, J. / Noh, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1805
-
Modeling of Crack Opening Displacement due to Delamination Using First-order Shear Laminate TheoryRoy, S. / Benjamin, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1816
-
Gas Permeability of Microcracked Laminates Under Cryogenic ConditionsAoki, T. / Ishikawa, T. / Yokozeki, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1824
-
An Investigation into the Global Dynamics of a Buckled Beam in the Case of a One-to-One Internal ResonanceNayfeh, A. / Emam, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1835
-
Component Mode Synthesis of a Vehicle System Model Using the Fictitious Mass MethodKarpel, M. / Moulin, B. / Feldgun, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1845
-
Bending Dominated Beam Dynamics: Continuous Shape Functions, Boundary Conditions and Internal LoadsHaering, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1856
-
Practical Application of the Rayleigh-Ritz Method to Verify Launch Vehicle Bending ModesIrvine, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1866
-
Dynamical Response Analysis of Jointed Structures by 2-D/3-D Adjusted Iwan Beam ElementsSong, Y. / Hartwigsen, C. / Bergman, L. / Vakakis, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1877
-
Dynamic Stiffness Formulation for Beams Undergoing Free Transverse and Lateral Vibration with Torsional CouplingBanerjee, R. / Su, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1885
-
Multiscale Modeling and Simulation of Grain Boundary EvolutionTa asan, S. / Yu, P. / Kinderlehrer, D. / Lee, J. / Livshits, I. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1894
-
Size and Strain Rate Effects in Tensile Deformation of CU NanowiresZhou, M. / Liang, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1901
-
MD Simulation of Grain Boundary Fracture in Copper and Connections to Interface Separation PotentialsSpearot, D. / McDowell, D. / Jacob, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1911
-
A Multiscale Modeling Approach to Crack Initiation in Metallic PolycrystalsIesulauro, E. / Ingraffea, A. / Heber, G. / Wawrzynek, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1919
-
Direct Numerical Simulation of PolycrystalsRadovitzky, R. / Cuitino, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1928
-
A Multiscale Approach to Modeling Fracture in Metallic Materials Containing Nonmetallic InclusionsGlaessgen, E. / Phillips, D. / Iesulauro, E. / Saether, E. / Piascik, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1938
-
Assessment of Structural Dynamic Model Accuracy Relative to Stochastic System BehaviorPaez, T. / Urbina, A. / Hasselman, T. / Wathugala, W. / Yep, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1949
-
Dynamic Behavior of Circular Structural Elements Under Thermal LoadsNayfeh, A. / Faris, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1958
-
Studies in Dynamic Analysis of Multi-body SystemsEbrahimi, N. / Hart, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1966
-
A Generalized Class of Energy Conservation/Dissipation [GlnO] Family of Time Operators with Improved Physical Attributes for Non-linear ComputationalKanapady, R. / Tamma, K. / Sandhu, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1977
-
The Reliability of the Arc-Length Method in the Analysis of Mode-Jumping ProblemsCerini, M. / Falzon, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 1987
-
Full-Field Structural Response of Composite Structures: Analysis and ExperimentMcGowan, D. / Ambur, D. / McNeill, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2004
-
Modeling the Structural Response of Multifunctional Materials: The In-field Vibration of Thin PlatesHarik, V. / Ounaies, Z. / Librescu, L. / Ambur, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2015
-
A Fuzzy Approach to Fiber-Reinforced Composite Material MechanicsRao, S. / Liu, Q. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2025
-
Structural Shape Identification from Experimental Strains Using a Modal Transformation TechniqueBogert, P. / Haugse, E. / Gehrki, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2043
-
Analytical Optimisation of Composite Cylindrical Shells to Meet Given Cross Sectional Stiffness PropertiesLemanski, S. / Weaver, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2050
-
Optimal Design of Tension Truss AntennasTibert, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2060
-
Design Optimization of Structural Acoustic Problems Using FEM-BEMKim, N. / Choi, K. / Dong, J. / Pierre, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2069
-
Probabilistic Design Optimization of Aircraft Structures with Reliability, Manufacturability, and Cost ConstraintsRais-Rohani, M. / Xie, Q. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2087
-
Piezoresistive Microphone Design Pareto Optimization: Tradeoff Between Sensitivity and Noise FloorPapila, M. / Haftka, R. / Nishida, T. / Sheplak, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2099
-
Optimal Design of an Electrostatically Actuated Micro-Beam for Maximum Pull-In VoltageReddy, C. / Faris, W. / Gurdal, Z. / Abdalla, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2106
-
Eulerian Shape Design Optimization with Fixed GridKim, N. / Chang, Y. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2114
-
Analytical and Experimental Investigations of the Active Stiffener Concept for Shape Control of a Circular Plate StructurePhilen, M. / Wang, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2125
-
Actuation, Sensing and Shape Control of a Smart Beam Using a General Electro-thermo-elastic FormulationVenkatesan, C. / Ahmad, S. / Upadhyay, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2136
-
Force-Deflection Behavior of a Smart Attachment MechanismClement, J. / Brei, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2151
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A Nonlinear Transmission that Increases Piezo-Stack Work OutputLesieutre, G. / Loverich, J. / Koopmann, G. / Mockensturm, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2162
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Design Model for Piezohydraulic ActuatorRegelbrugge, M. / Lindler, J. / Anderson, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2171
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Performance Modeling of a Piezohydraulic ActuatorSirohi, J. / Cadou, C. / Chopra, I. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2184
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System Identification of the SUITE Isolation Platform: Ground and Flight Experiment ComparisonBabuska, V. / Erwin, R. / Sullivan, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2195
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Payload Pointing and Active Vibration Isolation Using Hexapod PlatformsChen, H. / Bishop, R. / Agrawal, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2214
-
Vibration Testing and Control of an Inflatable Torus Using Multiple Sensors/actuatorsInman, D. / Sodano, H. / Park, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2222
-
Design and Characterization of a Compact Impact Damper for High Impulsive LoadsFacey, W. / Rosenfeld, N. / Wereley, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2232
-
Performance and Sensitivity Study on Sensoriactuator Circuits for Positive-real Damping SchemesKozlowski, M. / Cole, D. / Clark, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2243
-
Approximations in Bingham Plastic Analysis of Electrorheological and Magnetorheological DampersYoo, J. / Wereley, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2254
-
Optimal Control of Beam Dynamics with Segmented Photostrictive ActuatorsShih, H. / McLin, K. / Tzou, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2261
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Inflatably Deployed Membrane Waveguide Array Antenna for SpaceLichodziejewski, D. / Cravey, R. / Hopkins, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2268
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Thermal Distortion Analyses of a Three-Meter Inflatable Reflectarray AntennaFang, H. / Lou, M. / Huang, J. / Quijiano, U. / Hsia, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2278
-
Advanced Precipitation Radar Antenna Singly Curved Parabolic Antenna Reflector DevelopmentLin, J. / Scarborough, S. / Sapna, G. / Lopez, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2288
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Shaping of Parabolic Cylindrical Membrane Reflectors for the DART Precision Test BedWhite, C. / Salama, M. / Dragovan, M. / Hatheway, A. / Schroeder, J. / Dooley, J. / Barber, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2297
-
Selecting Models to Predict the Optical-Level Behavior of Membrane Primary MirrorsdeBlonk, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2308
-
Parametric Study of Net-Shape Membrane AperturesJenkins, C. / Wilkes, J. / Pilli, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2319
-
Probabilistic Design of Aerospace Vehicles: Coupling Global and Local RequirementsMahadevan, S. / Smith, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2328
-
On the Exploitation of Sensitivity Derivatives for Improving Sampling MethodsZang, T. / Cao, Y. / Hussaini, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2337
-
Reliability-based Design Optimization Using Probabilistic Safety FactorQu, X. / Haftka, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2349
-
Probabilistic Design Using Empirical DistributionsHajela, P. / Vittal, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2360
-
A State Transition Approach to Reliability Based Design and OptimizationHajela, P. / Vittal, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2371
-
Prognostics-Based Probabilistic Fatigue Life PredictionEnright, M. / Hudak, S. / McClung, C. / Millwater, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2380
-
Numerical Modeling of Creep/Damage Polymer Matrix Composites with Transverse IsotropyBinienda, W. / Robinson, D. / Acharya, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2385
-
RLV Thrust Cell Liner Coating Analysis and Design ConsiderationsButler, D. / Aboudi, J. / Arnold, S. / Pindera, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2396
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On the Mechanics of Composite Sinusoidal Honeycomb CoresQiao, P. / Wang, J. / Hu, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2405
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Reentry Flight and Ground Testing Experience with Hot Structures of C/C-SiC MaterialHald, H. / Ullmann, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2415
-
Variable Screening in Metamodel Design by Cross-Validated Moving Least Squares MethodTu, J. / Jones, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2424
-
Homotopy Curve Tracking in Approximate Interior Point OptimizationRenaud, J. / Perez, V. / Watson, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2435
-
A Practical Global Optimization ProcedureZhang, S. / Yu, X. / Johnson, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2449
-
Estimating the Error in Simulation Prediction Over the Design SpaceHemez, F. / Doebling, S. / Shinn, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2460
-
A Computationally Efficient Meshless Local Petrov-Galerkin Method for Axisymmetric ProblemsChen, T. / Raju, I. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2474
-
Meshless Local Petrov-Galerkin Euler-Bernoulli Beam Problems: A Radial Basis Function ApproachRaju, I. / Phillips, D. / Krishnamurthy, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2488
-
Parallel Numerical Simulation on Crack Propagation of Aeronautical StructuresKim, S. / Chung, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2495
-
Numerical Modelling of Fibre Metal Laminates Under Thermomechanical LoadingHagenbeek, M. / Remmers, J. / de Borst, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2504
-
Displacement Welding Technique for Coupled Analysis of Independently Modeled Finite Element SubstructuresCho, J. / Jee, Y. / An, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2513
-
Cohesive-Decohesive Interfacial Constitutive Law for the Analyses of Fatigue Crack Initiation and GrowthJohnson, E. / Goyal, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2524
-
Enhanced Structural Damage Tolerance of CFRP Primary Structures by Z-Pin ReinforcementClarke, A. / Greenhalgh, E. / Meeks, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2535
-
The Performance of Post-Buckled CFRP Stringer-Stiffened Panels Containing Defects and DamageGreenhalgh, E. / Meeks, C. / Clarke, A. / Thatcher, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2546
-
High Frequency, High Temperature Fretting Fatigue InvestigationsMatlik, J. / Farris, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2555
-
Fractographic Characteristics Associated with Fretting Fatigue Cracks in Turbomachinery AlloysGarcia, D. / Grandt, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2563
-
Dynamic Analysis for Delaminated Composites Using DKQ Concept Based on Higher-Order Zig-Zag TheoryCho, M. / Oh, J. / Kim, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2572
-
Active Structures Using Buckling Beam ActuatorsMockensturm, E. / Jiang, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2578
-
Design of Multi-Degree-of-Freedom Tuned-Mass Dampers Based on Eigenvalue PerturbationNayfeh, S. / Verdirame, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2589
-
Pendulation Reduction on Small Ship-Mounted Telescopic CranesMasoud, Z. / Nayfeh, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2595
-
Subharmonic Resonance of a MEMS Resonator Under Electric ActuationNayfeh, A. / Abdel-Rahman, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2603
-
The Effect of a Hard Coating on the Damping and Fatigue Life of TitaniumPalazotto, A. / Cross, C. / Ivancic, F. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2613
-
Circular Cylindrical Shells Immersed in a Magnetic Field: Modeling and Dynamic BehaviorLibrescu, L. / Hasanyan, D. / Ambur, D. / Qin, Z. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2623
-
A New Lagrangian-Eulerian Shell-Fluid Coupling Algorithm Based on Level SetsCirak, F. / Radovitzky, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2628
-
Spectral Element Model for the Vibration of an Axially Moving Timoshenko BeamLee, U. / Oh, H. / Kim, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2638
-
On the Transfer of Energy Between Widely Spaced ModesNayfeh, A. / Malatkar, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2649
-
A Novel Explicit Primal-Dual Based Time Stepping Method for Flexible Multibody Dynamical Systems of Index 3 in Semi-Explicit FormKanapady, R. / Sandhu, S. / Tamma, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2660
-
Integrated Stability Analysis of Large Space Structures Based on Potential Energy ConsiderationIshimura, K. / Natori, M. / Higuchi, K. / Wada, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2666
-
Genetic Algorithms in Decomposition Based Multicriteria OptimizationRyoo, J. / Hajela, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2677
-
Parallel Hierarchical Evolutionary Algorithms for Multicriteria Design Optimization Problems in Aerospace EngineeringWang, J. / Wu, Y. / Periaux, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2685
-
Minimum Weight Optimization of Composite Stiffened Panels Using Neural NetworksLanzi, L. / Bisagni, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2696
-
Design Optimization Using Fast Annealing Evolution AlgorithmsWang, B. / Pham, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2720
-
A Genetic Algorithm for Mixed Nonlinear Programming Problems Using Separate Constraint ApproximationsGantovnik, V. / Gurdal, Z. / Watson, L. / Anderson-Cook, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2727
-
The Effect of Chemical Functionalization on Mechanical Properties of Nanotube/Polymer CompositesOdegard, G. / Frankland, S. / Gates, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2741
-
Macroscale Experimental Evidence of a Reduced-mobility Non-bulk Polymer Phase in Nanotube-reinforced PolymersFisher, F. / Brinson, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2746
-
Carbon Nanofiber/Polymer Composites by Low Shear CompoundingLake, M. / Jacobsen, R. / Kwag, C. / van Hattum, F. / Burton, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2750
-
Process Investigation of Carbon Nanotube Bucky Paper/Epoxy NanocompositesZhang, C. / Wang, B. / Kramer, L. / Wang, Z. / Gou, J. / Liang, Z. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2760
-
Characterization and Modeling of the Fracture Behavior of Epoxy NanocompositesRoy, S. / Periasamy, S. / Ma, J. / Lu, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2770
-
Theoretical and Experimental Investigation of the Nonlinear Vibration of a Buckled Beam to a Subharmonic ResonanceNayfeh, A. / Emam, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2780
-
Nonlinear Responses of a Cantilever Wing with an External StoreKim, K. / Strganac, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2795
-
Nonlinear Sonic Fatigue Response Prediction from Finite Element Modal Models: A Comparison with ExperimentsGordon, R. / Spottswood, S. / Hollkamp, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2806
-
Nonlinear Response and Fatigue Life of Shallow Shells to Acoustic Excitation Using Finite ElementPrzekop, A. / Guo, X. / Azzouz, S. / Mei, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2818
-
A p-version Finite Element for Non-linear Vibration of Moderately Thick Laminated PlatesRibeiro, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2826
-
Nonlinear Vibration of Finitely Electroconductive Plate-Strips in a Magnetic FieldLibrescu, L. / Ambur, D. / Hasanyan, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2837
-
Affordability Comparison of Current and Adaptive and Multifuctional Air Vehicle SystemsBowman, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2846
-
Active Warping Control of a Joined Wing/Tail Airplane ConfigurationCesnik, C. / Brown, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2861
-
A Model to Compare the Flight Control Energy Requirements of Morphing and Conventionally Actuated WingsWiggins, L. / Robertshaw, H. / Mason, W. / Inman, D. / Johnston, C. / Neal, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2870
-
Synthesis of a Variable Geometry Trailing Edge Control SurfaceForster, E. / Sanders, B. / Eastep, F. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2881
-
Design of a Morphing Aspect Ratio Wing Using an Inflatable Telescoping SparBlondeau, J. / Richeson, J. / Pines, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2893
-
Impact of Strain Rate Dependent Viscosity on Damping Capacity of Electro- and Magnetorheological DampersWereley, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2902
-
Volume-Constrained Optimization of Magnetorheological ValvesRosenfeld, N. / Wereley, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2913
-
A Simultaneous Active-Passive Approach for Structural Vibration Confinement Using Piezoelectric ActuatorsTang, J. / Wang, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2924
-
Active Robust Shape Control of Flexible StructuresHu, Y. / Vukovich, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2934
-
Self-identification with Adaptive Gyroscopic Damper System Using Sensitivity AnalysesFuruya, H. / Senba, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2943
-
Combined Active and Passive Control of Space Structure Vibrations During LaunchJha, R. / Bailey, A. / Ahmadi, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2954
-
Computational Aeroelasticity: Success, Progress, ChallengeSchuster, D. / Liu, D. / Huttsell, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2977
-
Three-Dimensional Fluid-Structure Interactions of a Membrane Wing for Micro Air Vehicle ApplicationsLian, Y. / Shyy, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 2992
-
Predictions of Store-Induced Limit-Cylce Oscillations Using Euler and Navier-Stokes Fluid DynamicsSnyder, R. / Scott, J. / Khot, N. / Beran, P. / Zweber, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3003
-
Aeroelastic Response of a Delta Wing at High Angles of AttackGordnier, R. / Visbal, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3017
-
High-Order Finite Elements for Fluid/Structure Interaction ProblemsYosibash, Z. / Kirby, R. / Myers, K. / Szabo, B. / Karniadakis, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3025
-
Studies of Store-Induced Limit Cycle Oscillations Using a Model with Full System NonlinearitiesStrganac, T. / Kim, K. / Beran, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3039
-
Influence of Tip Store Mass Location on Wing Limit-Cycle OscillationKhot, N. / Beran, P. / Zweber, J. / Eastep, F. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3054
-
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback ControlYuan, Y. / Librescu, L. / Marzocca, P. / Yu, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3063
-
Nonlinear Response of Open/Closed-Loop Aeroelastic System Using a Discrete State-Space ApproachChen, P. / Sulaeman, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3074
-
Nonlinear Modeling of the Typical Section Immersed in Subsonic FlowRodrigues, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3094
-
A Study of a Prototype Actuator Concept for Membrane Boundary ControlHorta, L. / Panetta, A. / Solter, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3103
-
Vibration Studies of an Inflatable/Rigidizable Hexapod Structure with a Tensioned MembraneAdetona, O. / Horta, L. / Taleghani, B. / Blandino, J. / Woods, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3110
-
Approach for Efficiently Evaluating Internally Reacted Global Shape Control Actuation Strategies for AperturesFlint, E. / Denoyer, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3122
-
Modeling of an Active Seam AntennaJenkins, C. / Duvvuru, H. / Hossain, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3131
-
Development Studies of Thin Film TiNi-Polymeric Optical MembranesJardine, A. / Ho, K. / Carman, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3140
-
EAP Actuators for Controlling Space Inflatable StructuresTung, S. / Witherspoon, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3150
-
Structural Analysis and Testing of a 1/20th Scale NGST Sunshield Membrane LayerJohnston, J. / Blandino, J. / Black, J. / Pappa, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3160
-
Experimental Issues that Impact In-Vacuum Dynamic Characterization of Thin Film MembranesBales, G. / Hall, J. / Flint, E. / Glaese, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3169
-
Dynamic Characterization of a Subscale Solar Sail Using Non-Contacting Excitation and SensingSlade, K. / Belvin, W. / Tetlow, T. / Behun, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3180
-
Modal Identification of Membrane Structures with Videogrammetry and Laser VibrometryBlandino, J. / Pappa, R. / Black, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3191
-
Investigation of Structural Dynamics in a 2-meter Square Solar Sail Model Including Axial Load EffectsHolland, D. / Virgin, L. / Belvin, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3198
-
Nonlinear Vibration of Wrinkled MembranesPellegrino, S. / Kukathasan, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3209
-
Response Surface Approximation with Augmented and Compactly Supported Radial Basis FunctionsKrishnamurthy, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3224
-
Polynomial Chaos Expansion with Latin Hypercube Sampling for Predicting Response VariabilityChoi, S. / Grandhi, R. / Canfield, R. / Pettit, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3233
-
Stochastic Component Mode SynthesisBah, M. / Nair, P. / Bhaskar, A. / Keane, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3244
-
Assessment of the Efficiency of Partitioned Response Surface Equations in Structural ApplicationsVolovoi, V. / Zentner, J. / Mavris, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3251
-
Probabilistic Assessment on the Basis of Interval DataThacker, B. / Huyse, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3263
-
Anayltical Modeling of the High Strain Rate Deformation of Polymer Matrix CompositesGoldberg, R. / Roberts, G. / Gilat, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3272
-
Combined Experimental and Analytical Study of HCF in Turbine Blades Using Simplified GeometryPalazotto, A. / Patel, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3281
-
Ballistic Impact of Composite Plates and Half-Rings with Soft ProjectilesRoberts, G. / Pereira, J. / Revilock, D. / Binienda, W. / Xie, M. / Braley, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3290
-
Micro-Mechanical Modeling of the Adhesive Interface in Composite-Composite JointsLu, M. / Jenkins, C. / Winter, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3297
-
Composite Tank Permeation Prediction and VerificationAbdi, F. / Israeli, L. / Johnson, S. / Rayburn, J. / Aggarwal, P. / Fox, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3307
-
Accelerated Testing Methods for Next-Generation Launch VehiclesAbdi, F. / Huang, D. / Johnson, S. / Messinger, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3319
-
Thermo-Micromechanics of Microcracking in a Cryogenic Pressure VesselMallick, K. / Tupper, M. / Arritt, B. / Paul, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3329
-
Thermal-Mechanical Cyclic Test of a Composite Cryogenic Tank for Reusable Launch VehiclesMessinger, R. / Pulley, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3337
-
Temperature Effects on Resistivity of Mesoscopic Nanotube EnsemblesKoratkar, N. / Modi, A. / Suhr, J. / Lass, E. / Ajayan, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3345
-
Electrospun Electroactive Polymers for Actuator ApplicationsPawlowski, K. / StClair, T. / McReynolds, A. / Park, C. / Ounaies, Z. / Siochi, E. / Harrison, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3350
-
Nanostructured Materials for Rocket Propulsion System: Recent ProgressKoo, J. / Stretz, H. / Bray, A. / Weispfenning, J. / Luo, Z. / Blanski, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3361
-
Finite Deformation Continuum Model for Energetics of Carbon NanotubesGao, X. / Roy, A. / Li, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3367
-
Theoretical Interpretation of the Virial StressZhou, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3383
-
Multimode Large Amplitude Free Vibration of Shallow Shells Considering Inplane InertiaPrzekop, A. / Azzouz, S. / Guo, X. / Mei, C. / Azrar, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3394
-
Combined Delamination and Matrix Cracking in Adaptive Composite LaminatesThornburgh, R. / Chattopadhyay, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3405
-
Analysis of Bending Vibration of Rectangular Plates Using 2D Plate ModesWang, G. / Wereley, N. / Chang, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3416
-
Free Vibration Characteristics of Composite Shallow Circular Cylindrical Shells or Panels with a Non-Central Single Lap JointYuceoglu, U. / Ozerciyes, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3429
-
Fatigue Life Prediction for Panels Subjected to Thermo-Acoustic LoadingMignolet, M. / Spottswood, S. / Kim, K. / Yang, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3438
-
Decomposition Approach for Reliability-Based Multidisciplinary Design OptimizationRenaud, J. / Agarwal, H. / Mack, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3448
-
Trust Region Managed Reliability Based Design Optimization Using Evidence TheoryRenaud, J. / Preston, E. / Agarwal, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3463
-
Handling Equality Constraints in Robust Design OptimizationMessac, A. / Mattson, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3473
-
Experience with Approximate Reliability-Based Optimization MethodsYang, R. / Gu, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3481
-
Non-Gradient Based Methods for Probabilistic AnalysisWang, L. / Beeson, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3488
-
Design and Analysis of High-Frequency Periodically Layered Isolators for Helicopter Gearbox IsolationSzefi, J. / Smith, E. / Lesieutre, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3502
-
Rotorcraft Vibration and Noise Prediction Using a Unified Aeroelastic AnalysisFriedmann, P. / Liu, L. / Patt, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3516
-
Design and Performance Tests of Cycloidal Propulsion SystemsKim, S. / Yun, C. / Kim, D. / Yoon, Y. / Park, I. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3527
-
Design and Hover Test of Low Vibration Mach Scale Rotor with Twisted Composite Tailored BladeBao, J. / Nagaraj, V. / Chopra, I. / Bernhard, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3539
-
A Comprehensive Analysis for Whirl Flutter Stability of Two-Bladed Proprotor/Pylon SystemsSingh, B. / Chopra, I. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3554
-
Buckling of Long Compression-Loaded Anisotropic Plates Restrained Against Inplane Lateral and Shear DeformationsNemeth, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3591
-
Mode Jumping of an Isogrid Panel Under Quasi-static CompressionMuheim, D. / Johnson, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3602
-
Buckling Characteristics of Some Composite Stiffened Boxes Under Longitudinal Compression and Bending Using Finite Strip ApproachOvesy, H. / Assaee, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3611
-
Experiments on Axial Compression Postbuckling Behavior of Stiffened Cylindrical Composite PanelsAbramovich, H. / Grunwald, A. / Pevsner, P. / Weller, T. / David, A. / Ghilai, G. / Green, A. / Peker, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3621
-
Buckling Characteristics of a Plate with an Oblique Crack Under Tensile Loading - Elastic Buckling Analysis and ExperimentWakata, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3630
-
Post-Buckling Experimental Tests and Numerical Analyses on Composite Stiffened PanelsLanzi, L. / Bisagni, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3641
-
Flutter Suppression Using V-Stack Piezoelectric ActuatorArdelean, E. / McEver, M. / Clark, R. / Cole, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3650
-
Smart Spring - An Actively Tunable Vibration Absorber Designed to Control Aeroelastic ResponseNitzsche, F. / Wickramasinghe, V. / Zimcik, D. / Yong, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3658
-
Electromechanical Modeling of a Piezoelectric Actuator for Modulated/Vectored BlowingVasilescu, R. / Dancila, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3666
-
Development of Smart Spars for Active Aeroelastic StructuresCooper, J. / Amprikidis, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3677
-
Energy Perspectives in Aeroelastic ControlPatil, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3687
-
Inflatable and Rigidizable Wing Components for Unmanned Aerial VehiclesCadogan, D. / Smith, T. / Lee, R. / Graziosi, D. / Scarborough, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3695
-
Control of Sweep Using Pneumatic Actuators to Morph Wings of Small Scale UAVsde Marmier, P. / Wereley, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3706
-
Modeling Piezocomposite Actuators Embedded in Slender StructuresCesnik, C. / Palacios, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3717
-
Design of a Recurve Actuator for Maximum Energy EfiiciencyLindner, D. / Abdalla, M. / Gurdal, Z. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3723
-
Asymptotic Construction of a Thermopiezoelastic Model for Smart Composite PlatesHodges, D. / Yu, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3734
-
Shape Optimization of Electrodes for Piezoelectric ActuatorsWang, W. / Kurdila, A. / Venkataraman, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3745
-
Modelling and Sensitivity Analysis of a Variable Geometry Trailing Edge Control SurfaceForster, E. / Sanders, B. / Eastep, F. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3756
-
Neural and Conventional Adaptive Predictive Controllers for Smart StructuresJha, R. / He, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3767
-
Dynamic Buckling of Adaptive Composite ShellsChamis, C. / Abumeri, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3777
-
Fairing Noise Control Using Tube-Shaped ResonatorsLane, S. / Richard, R. / Kennedy, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3781
-
Adaptive Control for Interior Noise Control in Rocket FairingsMcEver, M. / Moon, S. / Clark, R. / Cole, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3791
-
Interaction Metrics for Feedback Control of Sound Radiation from Stiffened PanelsCabell, R. / Cox, D. / Gibbs, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3801
-
Active/Passive Control of Sound Radiation from Panels Using Constrained Layer DampingGibbs, G. / Cabell, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3808
-
Development of an Adaptive Passive Vibro-Acoustic Device for Payload FairingsHenderson, B. / Lane, S. / Griffin, S. / Lazzaro, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3813
-
Control of Noise Transmission into a Cylinder Using AdaptiveHelmholtz Resonators and Passive Vibration AbsorbersEsteve, S. / Johnson, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3823
-
Nonlinear AeroelasticityDowell, E. / Edwards, J. / Strganac, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3847
-
A Historical Perspective on Rotary Wing Dynamics and AeroelasticityFriedmann, P. / Hodges, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3890
-
Helicopter Performance and Vibration Enhancement by Twist-Actuated BladesShin, S. / Cesnik, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3901
-
Characterization and Modeling of Nonlinear Elastomeric Dampers Under Sinusoidal LoadingHu, W. / Wereley, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3912
-
Simulation of Elastomeric Damper Response Under Slowly Varying Amplitude ExcitationHu, W. / Wereley, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3922
-
Adaptive Neuro-Fuzzy Modeling of UH-60A Pilot VibrationKottapalli, S. / Langari, R. / Malki, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3931
-
Recent Developments in High Efficiency, Elastically Deployed Tubular TrussesWarren, P. / Hinkle, J. / Harvey, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3937
-
Elevated Temperature Mechanical Characterization of Isogrid BoomsScarborough, S. / Cadogan, D. / Pederson, L. / Blandino, J. / Steckel, G. / Stuckey, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3948
-
Buckling, Stiffness, and Modal Characterization of Foam-Rigidized Thin Film Deployable StructuresTinker, M. / Schnell, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3954
-
Load Analysis of Inflatable Truncated ConesVeldman, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3961
-
PowerSail: The Challenges of Large, Planar, Surface Structures for Space ApplicationsAdler, A. / Hague, N. / Spanjers, G. / Goodding, J. / Murphy, D. / Mikulas, M. / Engberg, B. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3970
-
An Articulated Motion and Vibration Isolator for SpacecraftMurphey, T. / Botke, M. / Blankinship, R. / Hague, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3982
-
Modeling the Dynamics of Large Diameter Doubly Curved Shells made from Thin-FilmsGlaese, R. / Regelbrugge, M. / Lore, K. / Smith, S. W. / Flint, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 3991
-
Experimentally Characterizing the Dynamics of 0.5m+ Diameter Doubly Curved Shells made from Thin FilmsFlint, E. / Bales, G. / Glaese, R. / Bradford, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4002
-
Modeling Pressure for Dynamic Analysis of an Inflatable StructureInman, D. / Jha, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4012
-
On a Probabilistic Strain-based Fatigue Life EstimationKolar, R. / Heffern, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4021
-
Probabilistic Sensitivity Analysis of Aircraft Damage Tolerance EstimatesMillwater, H. / Wieland, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4032
-
Application of an XML-based Database for Probabilistic AnalysisMillwater, H. / Fitch, S. / Enright, M. / Huyse, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4039
-
Efficient Statistical Analysis of Failure Risk in Engine Rotor Disks Using Importance Sampling TechniquesHuyse, L. / Enright, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4050
-
Probabilistic Fatigue of Integrally Stiffened Composite StructuresMinnetyan, L. / Chamis, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4059
-
Buckling of Long, Thin Inflatable Cylinders Loaded in Axial CompressionBreivik, N. / Watson, J. / Ambur, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4075
-
Towards a Probabilistic Preliminary Design Criterion for Buckling Critical Composite ShellsHilburger, M. / Arbocz, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4084
-
Shell Buckling Design Criteria Based on Manufacturing Imperfection SignaturesHilburger, M. / Nemeth, M. / Starnes, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4099
-
A Hierarchical High-Fidelity Analysis Procedure for Buckling Critical SructuresArbocz, J. / Starnes, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4118
-
Nonlinear Responses of Shallow Arches at VeeringNayfeh, A. / Lacarbonara, W. / Arafat, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4127
-
Stress Concentration and Failure Around Embedded Fiber Optic Sensor in Composite LaminatesBhargava, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4140
-
Micromechanical Bases for the Prediction of Failure of the Matrix in Fibrous CompositesParis, F. / Correa, E. / Mantic, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4151
-
Optimizing New Aluminum Alloys Through Computer Simulationvan der Veen, S. / Muzzolini, R. / Sigli, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4162
-
A Systematic Approach to Materials Information Management for Aerospace DesignMarsden, W. / Cebon, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4173
-
New Approaches to Materials EducationMarsden, W. / Ashby, M. / Cebon, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4179
-
Cure Analysis in Resin Transfer Molding of a Composite CylinderGolestanian, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4186
-
A Nonlinear 8-DOF Coupled Crane-Ship Dynamic ModelIdres, M. / Youssef, K. / Mook, D. / Nayfeh, A. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4197
-
Comparison of PDE/Galerkin and FEM for Non-linear Aerospace Structure AnalysesAzzouz, M. / Guo, X. / Przekop, A. / Mei, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4207
-
A Time Discontinuous Formulations Preserving a Consistent High-Order of Accuracy for Nonlinear/Linear Structural DynamicsKanapady, R. / Srinivasan, S. / Tamma, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4218
-
Stochastic Analysis of Nonlinear Viscoelastic Panels Under Random ExcitationPourtakdoust, S. / Assadian, N. / Fazelzadeh, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4225
-
Aerodynamic Design of Exo-skeletal Engine Fan BladesChamis, C. / Abumeri, G. / Schmidt, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4235
-
Structural Evaluation of Exoskeletal Engine Fan BladesChamis, C. / Kuguoglu, L. / Abumeri, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4245
-
Precise Roundness and Centrality Control of Thin ShellsBurge, J. / Duesler, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4255
-
Integrated Thermal/Mechanical Enhancements for Gas Turbine Engine CompressorsBurge, J. / Poire, N. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4263
-
Characterization of Modified Star Shape Cross-Sectional Beam Configurations with Rotorcraft ApplicationsHa, K. / Dancila, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4274
-
Design, Manufacturing and Testing of Elastically Tailored Composite Star Beam ConfigurationsKim, I. / Dancila, S. / Armanios, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4283
-
Nonlinear Time Delayed Feedback Control of Aeroelastic Systems: A Functional ApproachMarzocca, P. / Librescu, L. / Silva, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4294
-
Gantry Cranes Gain Scheduling Feedback Control with Friction CompensationNayfeh, A. / Omar, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4305
-
Energy-recycling Semi-active Method for Vibration Suppression with Piezoelectric TransducersOnoda, J. / Makihara, K. / Minesugi, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4316
-
Modeling and Validation of Damped Plexiglas Windows for Noise ControlBuehrle, R. / Gibbs, G. / Klos, J. / Mazur, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4326
-
Study of Electro Rheological Fluid Damper for Microgravity ExperimentWatanabe, K. / Yamakawa, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4332
-
Adaptive Structures for Microgravity Vibration Control and IsolationGattis, C. / Shepard, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4341
-
Umbilical Stiffness Matrix Characterization and Testing for Microgravity Science PayloadsEngberg, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4352
-
Mixed-Mode Fracture Toughness Tests for Stitched Composite LaminatesSankar, B. / Ifju, P. / Chen, L. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4363
-
Effect of Braid Angle and Waviness Ratio on Effective Moduli of 2x2 Biaxial Braided CompositesWhitcomb, J. / Goyal, D. / Kelkar, A. / Tang, X. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4373
-
Weaving Damage to Three-Dimensional Glass-Polymer CompositesMouritz, A. / Lee, L. / Rudov-Clark, S. / Bannister, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4382
-
F/A-18E/F Aeroservoelastic Design, Analysis, and TestPitt, D. / Hayes, B. / Goodman, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4392
-
X-32 AeroservoelasticityHunziker, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4397
-
Aeroservoelastic Design and Test of the X-45A Unmanned Combat Air VehicleReichenbach, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4404
-
A New Approach to Aeroservoelastic Aircraft ModellingIbrir, S. / Botez, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4410
-
Robust Stabilization of Uncertain Aircraft ModelsIbrir, S. / Botez, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4414
-
F/A-18 E/F Vertical Tail Buffet, Design, Analysis and TestHealey, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4426
-
Active Control of F/A-18 Vertical Tail Buffeting Using Piezoelectric ActuatorsSheta, E. / Moses, R. / Huttsell, L. / Harrand, V. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4437
-
Buffet Alleviation of F/A-18 Aircraft Using LEX FencesSheta, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4448
-
The Role of Buffet in the Structural Design of Eurofighter TyphoonLuber, W. / Becker, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4458
-
A Simple Technique for the Evaluation of Buffet Excitation ParameterWood, N. / Evans, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4464
-
A Brief History of Aircraft Loads Analysis MethodsTaylor, P. / Hanson, L. / Barnes, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4474
-
Identification of Critical Flight LoadsLove, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4484
-
A Systematic Approach to Evaluate The Effectiveness of Engine Mount SystemsLemire, J. / Rancourt, D. / Whiteford, G. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4494
-
A Descriptive Modeling and Simulation of Aircraft-Runway DynamicsRo, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4505
-
A Survey of Research Performed at NASA Langley Research Center's Impact Dynamics Research FacilityJackson, K. / Fasanella, E. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4524
-
Development, Design, and Testing of PowerSphere Multifunctional Ultraviolet-Rigidizable Inflatable StructuresSimburger, E. / Knoll, C. / Lin, J. / Rawal, S. / Perry, A. / Peterson, T. / Kerslake, T. / Curtis, H. / Matsumoto, J. / Giants, T. et al. | 2003
- 4535
-
Inflatable Rigidizable Solar Array for Small SatellitesLichodziejewski, D. / Veal, G. / Helms, R. / Freeland, R. / Kruer, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4542
-
Space Deployment of Inflatable Rigidizable Optical SphereGuidanean, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4551
-
Recent Developments in Inflatable Airbag Impact Attenuation Systems for Mars ExplorationStein, J. / Sandy, C. / Wilson, D. / Sharpe, G. / Knoll, C. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4557
-
Inflatable Structure: Development of a Recovery SystemBardet, C. / Briant, V. / Patanchon, G. / Granville, D. / Jetteur, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4567
-
Parachute Subsystems for the Beagle 2 Mars Lander Entry Descent and Landing SystemsLindstrand, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4569
-
Some Performance Trends in Hierarchical Truss StructuresMurphey, T. / Hinkle, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4584
-
Thermal-Structural Analysis of Sunshield MembranesJohnston, J. / Parrish, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4594
-
Evaluation of Cable Suspended Membrane Structures for Wrinkle-Free DesignSakamoto, H. / Miyazaki, Y. / Park, K. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4604
-
On the Precisely Uniform and Uniaxial Tensioning of a Film Sheet via Integrated CatenaryGreschik, G. / White, C. / Salama, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4615
-
A Rule of Thumb for the Suspension of Film Sheets Without CatenariesGreschik, G. / Murphey, T. / Mikulas, M. / Belvin, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4623
-
Deployment Characteristics of Creased Membrane for Solar Sail on Geometrical Configuration and Fold PatternFuruya, H. / Miyazaki, Y. / Takeuchi, H. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4630
-
A Stepwise Approach for Inflatable Space Equipment QualificationPeypoudat, V. / Roumeas, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4639
-
Fuzzy Finite Element Frequency Response Analysis of Structures with Uncertain ParametersVandepitte, D. / Moens, D. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4647
-
Competing Failure Risk Analysis Using Dempster-Shafer TheoryOberkampf, W. / Helton, J. / Johnson, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4670
-
Validation of Uncertainty Propagation ModelsMahadevan, S. / Rebba, R. / Zhang, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4678
-
Reliability of Laminated Composite Beams Subjected to Subtangential LoadsGoyal, V. / Kapania, R. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4695
-
Dynamic Creep Buckling of Viscoelastic Columns with Large Deformations and Follower Loads - Failure Probabilities and Survival TimesHilton, H. / Achour, M. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4706
-
Cylindrical Bending of Multilayered Magneto-Electro-Elastic PlatesPan, E. / Heyliger, P. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4714
-
A Transform Potential Theoretic Method for Acoustic Radiation from StructuresHariharan, S. / Sawyer, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4724
-
Analysis of Locally Irregular Composites Using the High-Fidelity Generalized Method of CellsPindera, M. / Aboudi, J. / Arnold, S. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4734
-
Characterization of Mode-II Fracture of Bi-Material Bonded Interfaces Using Tapered ENF SpecimenQiao, P. / Wang, J. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4746
-
Evaluation of Bending and Shear Moduli of Sandwich Structures by Dynamic Response Based TechniqueLestari, W. / Qiao, P. / Song, G. / Binienda, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4755
-
Aeroelastic System Development Using Proper Orthogonal Decomposition and Volterra TheoryLucia, D. / Beran, P. / Silva, W. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4767
-
Evaluation of CFL3D for Unsteady Pressure and Flutter PredictionsHong, M. / Kuruvila, G. / Bhatia, K. / SenGupta, G. / Kim, T. / American Institute of Aeronautics and Astronautics et al. | 2003
- 4778
-
A Harmonic Balance Approach for Modeling Nonlinear Aeroelastic Behavior of Wings in Transonic Viscous FlowThomas, J. / Hall, K. / Dowell, E. / American Institute of Aeronautics and Astronautics et al. | 2003