AIAA-2006-2058 System Design of Missile Based on CO with Variable Complexity Modeling (English)
- New search for: Lin, X.
- New search for: Yu, W. X.
- New search for: Li, Y.
- New search for: Qian, C. X.
- New search for: American Institute of Aeronautics and Astronautics
- New search for: Lin, X.
- New search for: Yu, W. X.
- New search for: Li, Y.
- New search for: Qian, C. X.
- New search for: American Institute of Aeronautics and Astronautics
In:
AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference
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5618-5624
;
2006
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ISBN:
- Conference paper / Print
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Title:AIAA-2006-2058 System Design of Missile Based on CO with Variable Complexity Modeling
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Contributors:Lin, X. ( author ) / Yu, W. X. ( author ) / Li, Y. ( author ) / Qian, C. X. ( author ) / American Institute of Aeronautics and Astronautics
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Conference:47th, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference ; 2006 ; Newport, R.I
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Published in:
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Publisher:
- New search for: American Institute of Aeronautics and Astronautics,
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Place of publication:Reston:
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Publication date:2006-01-01
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Size:7 pages
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Remarks:Paper numbers 2006-1600 to 2006-2284 with gaps held
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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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AIAA-2006-1600 Test and Analysis of an Inflatable Parabolic Dish AntennaGaspar, J. / Sreekantamurthy, T. / Mann, T. / Behun, V. / Romanofsky, R. / Lambert, K. / Pearson, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 18
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AIAA-2006-1601 Tape Spring Large Deployable AntennaSoykasap, O. / Pellegrino, S. / Howard, P. / Notter, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 30
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AIAA-2006-1602 Fabrication and Testing of Self-Deploying Foam Antenna StructuresHaight, A. H. / Rand, P. / Shkindel, T. / Allred, R. / McElroy, P. / Willis, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 42
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AIAA-2006-1603 Design Evaluation of a Large Aperture Deployable AntennaChodimella, S. / Moore, J. / Otto, J. / Fang, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 62
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AIAA-2006-1604 Concept Study of a 35-m Spherical Reflector System for NEXRAD in Space ApplicationLin, J. / Fang, H. / Im, E. / Quijano, U. / American Institute of Aeronautics and Astronautics et al. | 2006
- 74
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AIAA-2006-1605 Experimental Mechanics of a Wrinkled Multi-Layer Deployable Membrane Space AntennaHeald, J. / Potvin, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 85
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AIAA-2006-1608 An Automated Approach for Developing Discrete Adjoint SolversMartins, J. / Alonso, J. / van der Weide, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 95
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AIAA-2006-1609 Multidisciplinary Design Optimization for Aircraft ConfigurationsPuorger, P. C. / Mastroddi, F. / Pinna, F. / Bernardini, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 114
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AIAA-2006-1610 A Distributed Multi-Disciplinary Optimisation of a Blended Wing Body UAV Using a Multi-Agent Task EnvironmentBerends, J. / Tooren, M. / Belo, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 136
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AIAA-2006-1612 Multidisciplinary Design Optimization of UAV AirframesSobester, A. / Keane, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 149
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AIAA-2006-1613 An MDO Approach to Shape Optimization of Aerostat EnvelopesRam, C. V. / Pant, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 162
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AIAA-2006-1614 A Web-Based Interface for Complex Design Using a Virtual Engineering Software FrameworkKopecky, K. / Muth, D. / McCorkle, D. / Winer, E. / Bryden, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 171
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AIAA-2006-1616 AVEC: A Computational Design Framework for Conceptual InnovationsBlair, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 193
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AIAA-2006-1617 Comparison of MDO Architectures Within a Common Python FrameworkTedford, N. / Martins, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 212
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AIAA-2006-1618 A Web-Based Collaborative Environment for Bi-Level Integrated System Synthesis (BLISS)Kim, H. / Ragon, S. / Mullins, J. / Sobieszczanski-Sobieski, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 222
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AIAA-2006-1619 Roadmap for Moderate Fidelity Conceptual Design with Multilevel Analysis and MDOStriz, A. / Kennedy, B. / Siddique, Z. / Neeman, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 233
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AIAA-2006-1620 A System for Aerothermodynamic, Servo, Thermal, Elastic, Propulsive Coupled Analysis (ASTEP)Roughen, K. / Baker, M. / Seber, G. / Taylor, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 246
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AIAA-2006-1621 Optimal Control of LCOs in Aero-Structural SystemsPalaniappan, K. / Beran, P. / Jameson, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 253
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AIAA-2006-1622 Interactive Object-Oriented Model Builder for Structural and Aeroelastic Analysis and OptimizationKennedy, B. / Striz, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 263
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AIAA-2006-1623 Concurrent Shape Optimization of Structural ComponentsEdke, M. / Chang, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 274
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AIAA-2006-1624 Optimum Design of Structural Fuses for Robust and Predictable Progressive FailureSalas, P. / Venkataraman, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 295
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AIAA-2006-1625 A Fully Anisotropic Hierarchical Hybrid Cellular Automata Methodology to Simulate Bone RemodelingPenninger, C. / Patel, N. / Niebur, G. / Renaud, J. / Tovar, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 307
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AIAA-2006-1626 A Structural Design Optimization System Exploiting Distributed Grid ResourcesKere, P. / Lento, J. / Lyly, M. / Teras, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 316
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AIAA-2006-1627 A Computer Code for Design Optimization of Steel Portal FramesHernandez, S. / Loscos, P. / Pereiro, J. / Fontan, A. / Perezzan, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 328
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AIAA-2006-1629 Tailored Designer Functionally Graded Materials for Minimizing Probabilistic Creep Buckling Failures in Linear Viscoelastic Columns with Large Deformations and Follower LoadsHilton, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 345
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AIAA-2006-1630 A Non-Parametric Approach for Uncertainty Quantification in ElastodynamicsAdhikari, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 366
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AIAA-2006-1632 Taking Advantage of Separable Limit States in Sampling ProceduresSmarslok, B. / Haftka, R. / Kim, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 379
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AIAA-2006-1634 (Student Paper) Efficient Uncertainty Quantification in Computational Fluid-Structure InteractionsLoeven, G. / Witteveen, J. / Bijl, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 397
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Transonic limit cycle flutter of high-aspect-ratio swept wingsBendiksen, Oddvar O. et al. | 2006
- 397
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AIAA-2006-1635 Transonic Limit Cycle Flutter of High-Aspect-Ratio Swept WingsBendiksen, O. / American Institute of Aeronautics and Astronautics et al. | 2006
- 412
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AIAA-2006-1636 Dynamic Response of Highly Flexible Flying WingsSu, W. / Cesnik, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 436
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AIAA-2006-1637 Nonlinear Aeroelastic Response of the Flexible Wing in TrimNichkawde, C. / Strganac, T. / Beran, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 456
-
AIAA-2006-1638 Gust Response of Highly Flexible AircraftPatil, M. / Taylor, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 469
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AIAA-2006-1639 Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized ForcesDemasi, L. / Livne, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 488
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AIAA-2006-1640 Time Domain Nonlinear Aeroelastic Analysis for HALE WingsWang, Z. / Chen, P. / Liu, D. / Mook, D. / Patil, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 507
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AIAA-2006-1641 Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVsTuzcu, I. / Marzocca, P. / Cestino, E. / Romeo, G. / Frulla, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 523
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Progressive failure modeling of laminates incorporating material and geometric nonlinearitiesBasu, Shiladitya / Waas, Anthony M. / Ambur, Damodar R. et al. | 2006
- 523
-
AIAA-2006-1642 Progressive Failure Modeling of Laminates Incorporating Material and Geometric NonlinearitiesBasu, S. / Waas, A. / Ambur, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 551
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AIAA-2006-1643 Progressive Failure Analysis of Composite Stiffened PanelsBednarcyk, B. / Yarrington, P. / Collier, C. / Arnold, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 562
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AIAA-2006-1644 Transverse Loading of a Graphite/Epoxy Iso Truss PanelLarson, G. / Jensen, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 577
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AIAA-2006-1645 A Novel Subdomainwise Modeling Approach for Analysis of Layered Composite StructuresMohite, P. / Upadhyay, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 591
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AIAA-2006-1647 An Asymptotically Correct Model for Initially Curved and Twisted Thin-Walled Composite BeamsRoy, S. / Yu, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 600
-
AIAA-2006-1648 Behavior of Elliptical Composite Cylinders in TorsionHaynie, W. / Hyer, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 627
-
AIAA-2006-1649 Underload Injection Effect on Optimal Overload Values for Crack Growth RetardationElshabasy, M. / Newman, B. / Yu, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 644
-
AIAA-2006-1650 Mean Stress Effect on Optimal Overload for Crack Mitigation in Aircraft PanelsElshabasy, M. / Newman, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 666
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AIAA-2006-1651 Analytical Development of Fatigue Crack Growth Curve Without Conducting ASTM E647 TestsFarahmand, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 674
-
AIAA-2006-1652 Fretting Fatigue Testing of Ti-17 at Elevated TemperaturesGean, M. / Farris, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 685
-
AIAA-2006-1654 Comparison of Stress Intensity Factors for Cracks at Countersunk HolesShi, G. / Bellinger, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 685
-
Comparison of stress intensity factors for cracks at countersunk holesSlu, G. / Bellinger, N. et al. | 2006
- 695
-
Combustor featured fracture analysis and life predictionXiong, Yuexi / Dede, Mehmet / Venkitarama, Sundaram et al. | 2006
- 695
-
AIAA-2006-1655 Combustor Featured Fracture Analysis and Life PredictionXiong, Y. / Dede, M. / Venkitarama, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 706
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AIAA-2006-1656 Modeling of Ground Vibration Testing for Highly Flexible AircraftChang, C. / Hodges, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 728
-
AIAA-2006-1657 Experimentally Quantifying the Dynamic Response of Bolted Lap JointsPage, S. / Shiryayev, O. / Slater, J. / Pettit, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 740
-
AIAA-2006-1658 (Student Paper) Experimental Dynamic Response of a Solid Object to Various Diameter Low Pressure AirbagsDreher, P. / Canfield, R. / Maple, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 747
-
AIAA-2006-1659 Noise Separation Experiment for Flexible Structures Using Variable MassSenba, A. / Furuya, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 761
-
AIAA-2006-1660 Selection of a Location with Additional Mass and Stiffness in Component Modal TestsMisawa, M. / Matsuo, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 767
-
AIAA-2006-1661 Computational Modeling of Highly Flexible Membrane Wings in Micro Air VehiclesFerguson, L. / Aulisa, E. / Seshaiyer, P. / Gordnier, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 782
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AIAA-2006-1662 Nonlinear Deformations of Flapping Wings on a Micro Air VehicleBarut, A. / Das, M. / Madenci, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 807
-
AIAA-2006-1663 Dynamics of Insect-Based Flapping Wings: Loads ValidationSingh, B. / Chopra, I. / American Institute of Aeronautics and Astronautics et al. | 2006
- 833
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AIAA-2006-1664 Practical Large-Motion Modeling of Geometrically Complex Flexible VehiclesMcTavish, D. / Davidson, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 872
-
AIAA-2006-1665 Simulation of a Moving, Elastic Beam Using Hamilton's Weak PrincipleLeigh, E. / Kunz, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 883
-
Evaluation of precracking methods for the end-notched flexure testPerez, Carlos L. / Davidson, Barry D. et al. | 2006
- 883
-
AIAA-2006-1667 Evaluation of Precracking Methods for the End Notched Flexure TestPerez, C. / Davidson, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 898
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AIAA-2006-1668 Variability in Mixed-Mode Delamination Toughness with Implications for Research and Practical ApplicationsTeller, S. / Davidson, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 912
-
AIAA-2006-1669 Convective Heat Transfer in Open-Cell Metal Foams for Actively Cooled Thermal Protection SystemsSalas, K. / Waas, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 912
-
Convective heat transfer in open-cell metal foamsSalas, Ken I. / Waas, Anthony M. et al. | 2006
- 931
-
AIAA-2006-1671 Structural Design and Test of a Micro-Rocket Combustion ChamberNoonan, E. / Spearing, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 941
-
AIAA-2006-1672 Effect of Fiber Properties on Non-Linearity in 2x2 Biaxial Braided CompositesGoyal, D. / Whitcomb, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 956
-
AIAA-2006-1673 Fatigue Response of Joint Between Titanium and Titanium Matrix CompositeMall, S. / Cunningham, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 959
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AIAA-2006-1674 Multiscale Modeling of Grain-Boundary Fracture: Cohesive Zone Models Parameterized from Atomistic SimulationsGlaessgen, E. / Saether, E. / Phillips, D. / Yamakov, V. / American Institute of Aeronautics and Astronautics et al. | 2006
- 971
-
AIAA-2006-1675 Multiscale Modeling of Polymer Materials at Cryogenic and Elevated TemperaturesValavala, P. / Odegard, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 984
-
AIAA-2006-1676 Multiscale Analysis of Delamination of Carbon Fiber Epoxy Laminates with Carbon NanotubesRiddick, J. / Frankland, S. / Gates, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 984
-
Multiscale analysis of delamination of carbon fiber-epoxy laminates with carbon nanotubesRiddick, J.C. / Frankland, S.J.V. / Gates, T.S. et al. | 2006
- 996
-
AIAA-2006-1677 Modeling of Interface Behavior in Carbon Nanotube CompositesAwasthi, A. / Lagoudas, D. / Hammerand, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1005
-
Micromechanics modeling of functionally graded interphase regions in carbon nanotube-polymer compositesSeidel, Gary D. / Lagoudas, Dimitris C. / Frankland, Sarah Jane V. / Gates, Thomas S. et al. | 2006
- 1005
-
AIAA-2006-1678 Micromechanics Modeling of Functionally Graded Interphase Regions in Carbon Nanotube-Polymer CompositesSeidel, G. / Lagoudas, D. / Frankland, S. / Gates, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1020
-
AIAA-2006-1679 Study of Stress-strain Behavior of Carbon-nanotube Reinforced Epon 862 Composites Using Molecular DynamicsZhu, R. / Pan, E. / Roy, A. / Pan, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1027
-
AIAA-2006-1680 A Rigorous Finite Element Study on the Mechanical Properties of Single-Walled Carbon NanotubesMahdavi, A. / Mockensturm, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1027
-
A rigorous finite element study on the mechanical properties of single-walled carbon nanotubesMahdavi, Arash / Mockensturm, Eric et al. | 2006
- 1044
-
Development of deployable elastic composite shape memory alloy reinforced (DECSMAR) structuresPollard, Eric L. / Murphey, Thomas W. et al. | 2006
- 1044
-
AIAA-2006-1681 Development of Deployable Elastic Composite Shape Memory Alloy Reinforced (DECSMAR) StructuresPollard, E. / Murphey, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1062
-
AIAA-2006-1682 Development of Concentrated Strain Based Deployable Truss StructuresPollard, E. / Murphey, T. / Mejia-Ariza, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1075
-
AIAA-2006-1683 Analysis of the Lenticular Jointed MARSIS Antenna DeploymentMobrem, M. / Adams, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1088
-
AIAA-2006-1684 MARSIS Antenna Flight Deployment Anomaly and ResolutionAdams, D. / Mobrem, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1097
-
AIAA-2006-1685 Self-Locking Bi-Stable Deployable BoomsYou, Z. / Cole, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1107
-
AIAA-2006-1686 Manufacture and Experimental Analysis of a Concentrated Strain Based Deployable Truss StructureMejia-Ariza, J. / Murphey, T. / Pollard, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1117
-
AIAA-2006-1687 Minimum-Mass Design of Large Scale Space Trusses Subjected to Thermal GradientsWilliams, B. / Agnes, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1138
-
Mechanical and thermal behaviors of triaxially-woven carbon/epoxy fabric compositeAoki, Takahira / Yoshida, Keishiro et al. | 2006
- 1138
-
AIAA-2006-1688 Mechanical and Thermal Behaviors of Triaxially-Woven Carbon/Epoxy Fabric CompositeAoki, T. / Yoshida, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1147
-
A 3D micromechanics model for strain rate dependent inelastic polymer matrix compositesZhu, Linfa / Chattopadhyay, Aditi / Goldberg, Robert K. et al. | 2006
- 1147
-
AIAA-2006-1689 A 3D Micromechanics Model for Strain Rate Dependent Inelastic Polymer Matrix CompositesZhu, L. / Chattopadhyay, A. / Goldberg, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1165
-
A four cell decomposition model for unbalanced woven fabric composites subjected to thermal-mechanical loadingLua, Jim / Sankar, Jag / Pai, Devdas et al. | 2006
- 1165
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AIAA-2006-1690 A Four-Cell Decomposition Model for Unbalanced Woven Fabric Composites Subjected to Thermal-Mechanical LoadingLua, J. / Sankar, J. / Pai, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1186
-
AIAA-2006-1691 MLPG Formulation for Generalized Plane Strain Problems with Material Discontinuity and Application to Composite MicromechanicsDang, T. / Sankar, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1186
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MLPG formulation for generalized plane strain problems with material discontinuity and application to composite micromechanicsDang, Thi-D. / Sankar, Bhavani V. et al. | 2006
- 1204
-
A simple homogenization of degraded micro-cracked plain woven and braided textile compositesHur, Hae-Kyu / Johnson, Eric R. / Kapania, Rakesh K. et al. | 2006
- 1204
-
AIAA-2006-1692 A Simple Homogenization of Degraded Micro-Cracked Plain Woven and Braided Textile CompositesHur, H. / Johnson, E. / Kapania, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1230
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AIAA-2006-1693 After-Impact Compressive Strength Prediction for Laminated CompositesNguyen, T. / Zhao, Y. / Hill, E. / Wang, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1236
-
AIAA-2006-1694 A Study of Impacted Electromechanically Loaded Composite PlatesZhupanska, O. / Sierakowski, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1255
-
AIAA-2006-1695 Design and Fabrication of Light Rigidizable Inflatable WingsHaight, A. H. / Allred, R. / Harrah, L. / McElroy, P. / Scarborough, S. / Smith, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1264
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AIAA-2006-1696 A High-Altitude Test of Inflatable Wings for Low-Density Flight ApplicationsSmith, S. / Jacob, J. / Jones, R. / Scarborough, S. / Cadogan, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1277
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AIAA-2006-1697 Development of a Finite Element Model of Warping Inflatable WingsRowe, J. / Smith, S. / Simpson, A. / Jacob, J. / Scarborough, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1295
-
AIAA-2006-1698 Ultra Lightweight Ballutes for Return to Earth from MoonMasciarelli, J. / Lin, J. / Rohrschneider, R. / Bartels, R. / Hall, J. / Ware, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1303
-
AIAA-2006-1699 Structural Analysis and Testing of the Inflatable Re-Entry Vehicle Experiment (IRVE)Lindell, M. / Hughes, S. / Dixon, M. / Willey, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1322
-
AIAA-2006-1700 Concept of Inflatable Tensegrity for Large Space StructuresFuruya, H. / Murata, S. / Nakahara, M. / Jodoi, D. / Terada, Y. / Takadama, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1331
-
AIAA-2006-1701 Static, Buckling and Dynamic Behavior of Inflatable BeamsRendall, T. / Cormier, C. / Marzocca, P. / Jha, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1349
-
AIAA-2006-1702 Comparison of Advanced Propulsion Concepts for Interplanetary Exploration: Solar Sails, Rocks and Electric PropulsionDuffy, B. / Mazzoleni, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1369
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AIAA-2006-1703 Solar Sail Scalability and the Concept of a Truly Scalable ArchitectureGreschik, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1379
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AIAA-2006-1704 (Student Paper) Attitude Dynamics and Stability of Solar Sails During DeploymentLeFevre, B. / Jha, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1394
-
AIAA-2006-1705 Vaccum Deployment and Testing of a 20M Solar Sail SystemLichodziejewski, D. / Derbes, B. / Sleight, D. / Mann, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1408
-
AIAA-2006-1706 Structural Analysis and Test Comparison of a 20-Meter Inflation-Deployed Solar SailSleight, D. / Mann, T. / Lichodziejewski, D. / Derbes, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1424
-
AIAA-2006-1707 Ground Testing a 20-Meter Inflation Deployed Solar SailMann, T. / Behun, V. / Lichodziejewski, D. / Derbes, B. / Sleight, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1432
-
AIAA-2006-1708 Solar Sail Topology Variations Due to On-Orbit Thermal EffectsBanik, J. / Lively, P. / Taleghani, B. / Jenkins, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1452
-
AIAA-2006-1709 Controlling Structural Failure Modes During an Impact in the Presence of UncertaintiesMissoum, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1465
-
AIAA-2006-1710 Multilevel Hierarchical Decomposition: Identification Procedures for Edge of Design Space FeasibilitySomanath, N. / Staubach, J. / Midgeley, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1481
-
AIAA-2006-1711 Collaborative Optimization Framework Based on the Interaction of Low- and High-Fidelity Models and the Moving Least Squares MethodZadeh, P. / Toropov, V. / Wood, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1495
-
AIAA-2006-1712 Simultaneous Uniform DoEs for Model Building and Validation in the Multidisciplinary Optimization FrameworkNarayanan, A. / Toropov, V. / Wood, A. / Campean, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1507
-
AIAA-2006-1713 Collaboration Pursuing Method Using Latin Hypercube SamplingWang, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1514
-
AIAA-2006-1714 From Small X to Large X: Assessment of Space-Filling Criteria for the Design and Analysis of Computer ExperimentsGardner, M. / Ramanath, V. / Ayyalasomayajula, P. / Patterson, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1520
-
AIAA-2006-1715 Development of Repetitive Response Surface Enhancement Technique for the Multidisciplinary System OptimizationJeon, K. / Lee, J. / Byun, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1529
-
AIAA-2006-1716 Optimization of a Personnel Launch System for Space Tourism OperationsGarcia, E. / Pasqual, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1544
-
AIAA-2006-1717 Development, Structure, and Application of MAST: A Generic Mission Architecture Sizing ToolLafleur, J. / Restrepo, C. / Grant, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1555
-
AIAA-2006-1718 Multidisciplinary Design Optimization of Reentry Vehicles: Trajectory Optimization and SensitivitiesMor, M. / Livne, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1585
-
AIAA-2006-1720 Multiobjective Optimization of Two-Stage Rockets for Earth-to-Orbit LaunchBairstow, B. / de Weck, O. / Sobieszczanski-Sobieski, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1601
-
AIAA-2006-1721 Research on Theory and Application of Multidisciplinary Design Optimization of Flying VehiclesChen, X. / Yan, L. / Luo, W. / Xu, L. / Zhao, Y. / Wang, Z. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1625
-
AIAA-2006-1722 Mission and System Design of Air-Launching Rocket Using Multidisciplinary Optimization ApproachChoi, Y. / Noh, K. / Lee, J. / Byun, Y. / Yu, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1633
-
Nonparametric risk assessment of gas turbine enginesEnright, Michael P. / McClung, R.Craig / Hudak, Stephen J. et al. | 2006
- 1633
-
AIAA-2006-1725 Nonparametric Risk Assessment of Gas Turbine EnginesEnright, M. / McClung, C. / Hudak, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1642
-
AIAA-2006-1726 Towards Hardware Implementation of a Probabilistic Fatigue Algorithm for Engine Health MonitoringHan, Y. / Millwater, H. / Portillo, J. / John, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1642
-
Towards hardware implementation of a probabilistic fatigue algorithm for engine health monitoringHan, Young-Hoon / Millwater, H. / Portillo, John / John, E. et al. | 2006
- 1666
-
AIAA-2006-1728 Simulation and Classification of Random Multiphase Materials Through Short-Range CorrelationGraham-Brady, L. / Xu, X. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1675
-
Statistical analysis of effect of contact surface profile on fretting fatigue life for Ti-6Al-4VKumari, Shyama / Farris, Thomas N. et al. | 2006
- 1675
-
AIAA-2006-1729 Statistical Analysis of Effect of Surface Profile on Fretting Fatigue Life for Ti-6AL-4VKumari, S. / Farris, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1696
-
AIAA-2006-1730 Flutter of Partially Rigid Cantilevered Plates in Axial FlowDe Breuker, R. / Abdalla, M. / Gurdal, Z. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1710
-
AIAA-2006-1731 Aerothermoelastic Stability of Composite Aircraft Wings Subjected to Heat InputsPolli, G. / Mastroddi, F. / Librescu, L. / DiTrapani, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1710
-
Aerothermoelastic stability of composite aircraft wings subjected to heat inputsPolli, Gian Mario / Mastroddi, Franco / Librescu, Liviu / Di Trapani, Claudia et al. | 2006
- 1726
-
Finite element time domain - Modal formulation for nonlinear flutter of cylindrical panelsAzzouz, M.Salim / Mei, Chuh et al. | 2006
- 1726
-
AIAA-2006-1732 Finite Element Time Domain - Modal Formulation for Nonlinear Flutter of Composite Curved PanelsAzzouz, M. / Mei, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1754
-
AIAA-2006-1734 Nonlinear Aeroelastic Studies on a Folding Wing Configuration with Free-Play Hinge NonlinearityLee, D. / Chen, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1776
-
AIAA-2006-1736 Aeroelastic Analysis of an Airfoil with a Hysteresis Non-LinearityGu, Y. / Yang, Z. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1785
-
AIAA-2006-1737 Energy-Consistent, Galerkin Approach for the Nonlinear Dynamics of Beams Using Mixed, Intrinsic EquationsPatil, M. / Althoff, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1794
-
AIAA-2006-1739 Dynamics of Thin-Walled Composite Aircraft Wings Carrying External StoresLibrescu, L. / Song, O. / Kwon, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1808
-
AIAA-2006-1740 Free Vibration of a Three-Layered Sandwich Beam Using Theory and ExperimentBanerjee, R. / Cheung, C. / Morishima, R. / Perera, M. / Njuguna, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1830
-
AIAA-2006-1742 Finite Element Analysis of Beams with Nonlocal FoundationsLei, Y. / Friswell, M. / Adhikari, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1841
-
AIAA-2006-1744 Accurate Structural Dynamic Modeling of the Hunter UAV Using Ground Vibration TestingKosmatka, J. / Valdes, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1853
-
AIAA-2006-1745 Dynamic Snap Through of Thin-Walled Structures by a Reduced Order MethodPrzekop, A. / Rizzi, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1864
-
AIAA-2006-1746 A Reduction Method for Finite Elements Nonlinear Dynamic Analysis of ShellsTiso, P. / Jansen, E. / Abdalla, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1877
-
AIAA-2006-1747 Modified Generalized Alpha Method for Integrating Governing Equations of Very Flexible AircraftShearer, C. / Cesnik, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1898
-
AIAA-2006-1748 Component Effective Modal MassMajed, A. / Henkel, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1902
-
AIAA-2006-1749 Coons Patch, Hermite Interpolation and High-Order Finite Elements in Structural DynamicsMorino, L. / Cetta, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1919
-
AIAA-2006-1750 Comparison of Damage Path Predictions for Composite Laminates by Explicit and Standard Finite Element Analysis ToolsBogert, P. / Satyanarayana, A. / Chunchu, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1942
-
AIAA-2006-1751 Application of Linear Finite Elements to Finite Strain Using CorotationRankin, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1970
-
AIAA-2006-1753 (Student Paper) A New Finite Element for a Shear Deformable PlatePatel, H. / Shimpi, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1985
-
AIAA-2006-1754 An h-Adaptive Finite Element Technique for Linear Elastic Fracture ProblemsBisi, A. / Gopalakrishnan, S. / Dattaguru, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1998
-
AIAA-2006-1755 Application of Artificial Neural Networks to the Simulation of Progressive Damage in Composite LaminatesDeenadayalu, C. / Chattopadhyay, A. / Zhou, X. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2016
-
AIAA-2006-1756 A Large Deflection Model for Thin, Rectangular Plates Subjected to Blast LoadingFlorek, J. / Benaroya, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2024
-
AIAA-2006-1757 Experimental and Finite Element Analysis of Preloaded Bolted Joints Under Impact LoadingO Toole, B. / Karpanan, K. / Feghhi, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2033
-
AIAA-2006-1758 A Consistent Configuration Formulation Involving Continuum Damage Mechanics Based Lagrangian Hydrodynamic Computational Framework for 3D High- and HypZhou, X. / Sha, D. / Tamma, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2044
-
AIAA-2006-1759 Robust Bird-Strike Modeling Based on ALE Formulation Using LS-DYNAGoyal, V. / Huertas, C. / Borrero, J. / Leutwiler, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2062
-
AIAA-2006-1760 Channel Section Short Column with Fixed Ends Under Axial Impact LoadShoji, H. / Minegishi, M. / Aoki, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2077
-
AIAA-2006-1762 Simulation of Landing Events for an Unconventional UAV Landing Gear System Using Transient Dynamics ApproachNguyen, P. / Mak, S. / Panza, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2085
-
A review of classical fiber microbuckling analytical solutions for use with elastic memory compositesFrancis, William H. / Lake, Mark S. / Steven Mayes, J. et al. | 2006
- 2085
-
AIAA-2006-1764 A Review of Classical Fiber Microbuckling Analytical Solutions for use with Elastic Memory CompositesFrancis, W. / Lake, M. / Mayes, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2097
-
AIAA-2006-1765 Electric Field Patterning of Dielectric Particles in LiquidPolymersBoyd, J. / Lee, J. / Seo, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2097
-
Electric field patterning of dielectric particles in liquid polymersBoyd IV, James G. / Lee, Jaesang / Seo, Cheongsoo et al. | 2006
- 2106
-
AIAA-2006-1766 Modeling of the Stress- and Magnetic Field-Induced Variant Reorientation in MSMAsKiefer, B. / Lagoudas, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2121
-
AIAA-2006-1767 Processing of Light-Weight Shape Memory Alloys Using Spark Plasma SinteringMajkic, G. / Chen, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2126
-
AIAA-2006-1768 Dynamic Behavior of Ferromagnetic Shape Memory AlloysScoby, S. / Chen, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2130
-
AIAA-2006-1769 Properties of Ti50Ni25Cu25 Melt-Spun RibbonTong, Y. / Liu, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2136
-
Mechanical characterization and modeling of isocyanate-crosslinked nanostructured silica aerogelsRoy, Samit / Shimpi, Nilesh / Katti, Atul / Lu, Hongbing / Rahman, Mosfequr et al. | 2006
- 2136
-
AIAA-2006-1770 Mechanical Characterization and Modeling of Isocyanate-Crosslinked Nanostructured Silica AerogelsRoy, S. / Shimpi, N. / Katti, A. / Lu, H. / Rahman, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2162
-
AIAA-2006-1771 Prediction of Delamination Resistance in Laminated Composites with Electrospun Nano-Interlayers using a Cohesive Zone ModelSihn, S. / Park, J. / Kim, R. / Huh, W. / Roy, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2172
-
Facilitating interfacial slip in carbon nanotube polycarbonate compositesSuhr, Jonghwan / Koratkar, Nikhil A. et al. | 2006
- 2172
-
AIAA-2006-1772 Facilitating Interfacial Slip in Carbon Nanotube Polycarbonate CompositesSuhr, J. / Koratkar, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2179
-
AIAA-2006-1774 Elastic and Inelastic Behavior of Carbon Nanotube Reinforced PolystyreneKrzyzanowski, D. / Chattopadhyay, A. / Zhou, X. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2179
-
Elastic and inelastic behavior of carbon nanotube reinforced polystyreneKrzyzanowski, David R. / Chattopadhyay, Aditi / Zhou, Xu et al. | 2006
- 2187
-
AIAA-2006-1775 Impact Analysis of NanoCompositesAvila, A. / Duarte, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2187
-
Impact analysis of nanocompositesAvila, Antonio F. / Duarte, Horacio V. et al. | 2006
- 2198
-
AIAA-2006-1776 Phonon Engineering of Free and Embedded Nanocarbon Fragments: Heat Spreading and Nanosound PropagationGlushko, E. / Evteev, V. / Slusarenko, N. / Gurova, I. / Tarasov, I. / Zakhidov, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2215
-
AIAA-2006-1778 Development and Verification of a Probabilistic Model for Space Shuttle Debris TransportThacker, B. / Riha, D. / Pleming, J. / Huyse, L. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2229
-
AIAA-2006-1779 Computational and Analytical Modeling of Foam, Ice and Ablator Materials Impacting Space Shuttle Thermal TilesWalker, J. / Chocron, S. / Gray, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2242
-
AIAA-2006-1780 Thermal Protection System (TPS) Impact ExperimentsGrosch, D. / Bertrand, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2255
-
AIAA-2006-1781 Progressive Failure Analysis of Shuttle Reinforced Carbon-Carbon Plate SpecimensSokolinsky, V. / Housner, J. / Surdenas, J. / Abdi, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2261
-
AIAA-2006-1782 Fracture Mechanics Analysis of LH2 Feed Line Flow LinersJames, M. / Dawicke, D. / Brzowski, M. / Raju, I. / Elliot, K. / Harris, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2270
-
AIAA-2006-1783 A Probabilistic Return-to-Flight Assessment of the Orbiter's LH2 Feedline FlowlinerHudak, S. / Huyse, L. / Chell, G. / Lee, Y. / Riha, D. / Thacker, B. / McClung, C. / Gardner, B. / Pleming, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2286
-
AIAA-2006-1784 Buckling of Laminated Composite Plates via a Refined Higher-Order TheoryFiedler, L. / Lacarbonara, W. / Vestroni, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2286
-
Buckling of composite laminated plates via a refined higher-order theoryFiedler, Lars / Lacarbonara, Walter / Vestroni, Fabrizio et al. | 2006
- 2298
-
Buckling analysis of laminates with a cutout using a zeroth-order shear deformation theoryBarut, A. / Madenci, E. et al. | 2006
- 2298
-
AIAA-2006-1785 Buckling Analysis of Laminates with a Cutout Using a Zeroth-Order Shear Deformation TheoryBarut, A. / Madenci, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2328
-
A semi-analytical approach for predicting the post-buckling response of laminates with a cutoutBarut, A. / Madenci, E. et al. | 2006
- 2328
-
AIAA-2006-1786 A Semi-Analytical Approach for Predicting the Postbuckling Response of Laminates with a CutoutBarut, A. / Madenci, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2354
-
AIAA-2006-1787 Post-Buckling of Stiffened Composite Structures with DelaminationsKontis, N. / Butler, R. / Hunt, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2354
-
Post-buckling of stiffened composite structures with delaminationsKontis, N. / Butler, R. / Hunt, G.W. et al. | 2006
- 2369
-
AIAA-2006-1788 Prediction of Local, Global Buckling and Their Interactions on Thin Circular Cylindrical ShellsWong, K. / Weaver, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2382
-
The characterization of friction stir welding process effects on stiffened panel buckling performanceMurphy, A. / McCune, W. / Price, M. / Curran, R. / Quinn, D. / Wilson, R. et al. | 2006
- 2382
-
AIAA-2006-1789 The Characterization of Friction Stir Welding Process Effects on Stiffened Panel Buckling PerformanceMurphy, A. / McCune, W. / Price, M. / Curran, R. / Quinn, D. / Wilson, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2397
-
AIAA-2006-1790 Studies on Small Rectangular Membranes with Actuation Along the BoundaryKorde, U. / Jenkins, C. / Hofacker, M. / Farke, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2410
-
Reliability study of DEPP functionally graded actuatorsAlexander, Paul W. / Brei, Diann / Halloran, John W. et al. | 2006
- 2410
-
AIAA-2006-1791 Reliability Study of DEPP Functionally Graded Piezoceramic ActuatorsAlexander, P. / Brei, D. / Halloran, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2422
-
AIAA-2006-1792 (Student Paper) Experimental Verification of Models for Microfabricated Piezoelectric Vibration Energy HarvestersDuToit, N. / Wardle, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2442
-
AIAA-2006-1793 3-D Elasticity-based Modeling of Anisotropic Piezocomposite Transducers for Guided Wave Structural Health MonitoringRaghavan, A. / Cesnik, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2442
-
3-D elasticity-based modeling of anisotropic piezocomposite transducers for guided wave structural health monitoringRaghavan, Ajay / Cesnik, Carlos E.S. et al. | 2006
- 2461
-
AIAA-2006-1795 Nonlinear Semi-Analytical Modeling of Post-Buckled Precompressed (PBP) Piezoelectric Actuators for UAV Flight ControlDe Breuker, R. / Tiso, P. / Vos, R. / Barrett, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2474
-
AIAA-2006-1796 On the Design of Morphing Airfoils Using Spinal StructuresUrsache, N. / Keane, A. / Bressloff, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2484
-
AIAA-2006-1798 Effective Modulus of Creased Thin MembranesWoo, K. / Nandurkar, K. / Jenkins, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2497
-
AIAA-2006-1800 Sensivitity Analysis Method for Membrane Wrinkling Based on Projection OperatorAkita, T. / Natori, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2511
-
AIAA-2006-1801 Nonlinear Material Response of Systematically Creased MembranesHossain, N. / Woo, K. / Jenkins, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2529
-
AIAA-2006-1803 Computation of Buckling Pressure of Pumpkin BalloonsPagitz, M. / Pellegrino, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2551
-
AIAA-2006-1804 Experimental Validation of Close-Range Photogrammetric Measurement Performance of Doubly Curved SurfacesFlint, E. / Hall, J. / Lindler, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2565
-
Measurement of in-plane motion of thin-film structures using videogrammetryLeifer, Jack / Smith, Suzanne Weaver / Black, Jonathan T. / Ma, Ning / Lumpp, Janet K. et al. | 2006
- 2565
-
AIAA-2006-1805 Measurement of In-Plane Motion of Thin-Film Structures Using VideogrammetryLeifer, J. / Smith, S. / Black, J. / Ma, N. / Lumpp, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2581
-
AIAA-2006-1806 A Method for Assessing the Accuracy of a Photogrammetry System for Precision Deployable StructuresMoore, A. / Williams, R. / Agnes, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2589
-
AIAA-2006-1807 Developments in Superstring Deployable Truss BoomBrown, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2595
-
AIAA-2006-1808 Deploy Experiment of Inflatable Tube Using Work HardeningSenda, K. / Ohta, S. / Igarashi, Y. / Watanabe, A. / Hori, T. / Ito, H. / Tsunoda, H. / Watanabe, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2613
-
AIAA-2006-1809 Design and Evaluation of an Ultra-Light Extendible Mast as an Inflatable StructureHiguchi, K. / Watanabe, K. / Watanabe, A. / Tsunoda, H. / Yamakawa, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2620
-
AIAA-2006-1810 Neutrally Stable Composite Tape SpringsSchultz, M. / Hulse, M. / Keller, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2628
-
AIAA-2006-1811 A Comparison Meta-Modeling Methods Using Practical Industry RequirementsWang, L. / Beeson, D. / Wiggs, G. / Rayasam, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2653
-
AIAA-2006-1812 Model Accuracy Evaluation of Compactly Supported RBFsFang, H. / Wang, Q. / Horstemeyer, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2661
-
AIAA-2006-1813 Uncertainty Visualization in Multiobjective Robust Design OptimizationRangavajhala, S. / Mullur, A. / Messac, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2677
-
AIAA-2006-1814 Topology Optimization Using Hyper Radial Basis Function NetworkWang, B. / Apte, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2686
-
AIAA-2006-1815 Application of Response Surface Methodology to Stiffened Panel OptimizationMerval, A. / Samuelides, M. / Grihon, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2697
-
AIAA-2006-1817 Inverse Design Optimization of a Multistage Space Launch Vehicle Using Rough SetsQazi, M. / He, L. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2713
-
AIAA-2006-1818 Minimum Weight Design of Composite Wing Structures with Local Postbuckling and Blending ConstraintsSeresta, O. / Abdalla, M. / Gurdal, Z. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2747
-
AIAA-2006-1819 Strategies for Multifidelity Optimization with Variable Dimensional Hierarchical ModelsRobinson, T. / Eldred, M. / Willcox, K. / Haimes, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2766
-
AIAA-2006-1820 Airfoil Design and Optimization Using Multi-Fidelity Analysis and Embedded Inverse DesignBarrett, T. / Bressloff, N. / Keane, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2787
-
AIAA-2006-1821 Surrogate Based Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward FlightGlaz, B. / Friedmann, P. / Liu, L. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2808
-
AIAA-2006-1822 Coupling Global and Local Aspects of Cross-Sectional Optimization for Rotor BladesVolovoi, V. / Ku, J. / Hodges, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2822
-
AIAA-2006-1823 Design and Shape Optimization of Inflatable WingsMarzocca, P. / Gurdal, Z. / Hol, J. / Chang, C. / Crosbie, E. / Calder, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2832
-
AIAA-2006-1824 Combined Parallel Computing, Dynamic Mesh and Heuristic Algorithms in Tapered WingsVatandas, E. / Ozkol, I. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2843
-
AIAA-2006-1825 Tail Modeling in Reliability-Based Design Optimization for Highly Safe Structural SystemsKim, N. / Queipo, N. / Ramu, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2854
-
AIAA-2006-1826 A New Adaptive Ordinal Approach to Continuous-Variable Probabilistic OptimizationRomero, V. / Chen, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2873
-
AIAA-2006-1827 Evaluation of Sampling Methods in Constructing Response Surface ApproximationsSwiler, L. / Slepoy, R. / Giunta, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2897
-
AIAA-2006-1828 Second-Order Reliability Formulations in DAKOTA/UQEldred, M. / Bichon, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2920
-
AIAA-2006-1829 Progressive Importance Sampling Approach for Reliability AnalysisShin, Y. / Wu, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2928
-
AIAA-2006-1830 A Probabilistic Treatment of Expert Knowledge and Epistemic Uncertainty in NESSUSHuyse, L. / Thacker, B. / Riha, D. / Fitch, S. / Pepin, J. / Rodriguez, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2935
-
AIAA-2006-1831 Probabilistic Comparison of Four Different MethodsAbumeri, G. / Chamis, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2945
-
AIAA-2006-1832 Non Linear Aeroelastic Response and Control of Supersonic Flapped 2-D Lifting SurfacesMarzocca, P. / Librescu, L. / Na, S. / Rubillo, C. / Chan, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2960
-
AIAA-2006-1833 Active Alleviation of Gust Loads Using Special Control SurfacesKarpel, M. / Moulin, B. / Feldgun, V. / Anguita, L. / Rosich, F. / Climent, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2977
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AIAA-2006-1834 Control Structure Interaction Testbed: Passive Isolation, Simulation & TestBrennan, S. / Bronowicki, A. / Ryan, P. / Simonian, S. / Hurst, W. / McMonagle, R. / Sweeney, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 2994
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AIAA-2006-1835 Time-Delayed Feedback Control of a 2-D Supersonic Flapped WingsChen, Z. / Yu, P. / Marzocca, P. / Librescu, L. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3005
-
AIAA-2006-1836 Robust Aeroelastic Control of 2-D Supersonic Flapped Lifting SurfacesNa, S. / Librescu, L. / Marzocca, P. / Yoon, G. / Rubillo, C. / Bong, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3015
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AIAA-2006-1837 Active Control of Non-Linear Aeroelastic Response Using Conformal Control SurfacesMarques, F. / De Marqui, C. / Caixeta, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3025
-
Concurrent optimal design of piezoelectric actuators and controller for smart vibration controlJoshi, Kunal V. / Mujumdar, P.M. et al. | 2006
- 3025
-
AIAA-2006-1838 Concurrent Optimal Design of Piezoelectric Actuators and Controller for Active Vibration ControlJoshi, K. / Mujumdar, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3045
-
AIAA-2006-1839 Thermoelastic Cracked Cylindrical Shells Subjected to Nonstationary Electrical CurrentQin, Z. / Hasanyan, D. / Librescu, L. / Young, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3062
-
AIAA-2006-1840 Fire Damage Assessment of a Loaded Composite Sandwich Structure Subjected to a FireLua, J. / Wu, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3062
-
Fire damage assessment of a loaded composite sandwich structure subjected to a fireLua, Jim / Wu, Yongshu et al. | 2006
- 3091
-
AIAA-2006-1841 The Residual Strength of Composite Army Bridge After Fire ExposureQian, Z. / Abdi, F. / Miraj, R. / Mosallam, A. / Iyer, R. / Wang, J. / Logan, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3101
-
AIAA-2006-1842 Crack Growth Strategy in Composite Under Static LoadingXie, D. / Qian, Z. / Huang, D. / Abdi, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3109
-
AIAA-2006-1844 Safety Envelope for Load Tolerance and Its Application to Fatigue Reliability DesignWang, H. / Kim, N. / Kim, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3117
-
AIAA-2006-1846 Analysis of Store Effects on Limit-Cycle OscillationParker, G. / Maple, R. / Beran, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3137
-
AIAA-2006-1847 An Investigation of the Sensitivity of F-16 Fighter Flutter Onset and Limit Cycle Oscillations to UncertaintiesThomas, J. / Dowell, E. / Hall, K. / Denegri, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3145
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AIAA-2006-1848 Suppression of Limit Cycle Oscillations with a Nonlinear Energy Sink: Experimental ResultsHill, W. / Strganac, T. / Nichkawde, C. / McFarland, D. / Kerschen, G. / Lee, Y. / Vakakis, A. / Bergman, L. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3158
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AIAA-2006-1849 Suppression of Aeroelastic Instability with a Nonlinear Energy Sink: Theoretical BasisLee, Y. / Vakakis, A. / Bergman, L. / McFarland, D. / Kerschen, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3169
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AIAA-2006-1850 Limit Cycle Oscillation Prediction of Asymmetric External Store Configurations Using Neural NetworksDawson, K. / Maxwell, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3183
-
AIAA-2006-1851 Flight-Loads Effects on Free-Play Induced Limit Cycle OscillationChen, P. / Lee, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3196
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AIAA-2006-1852 Characterization of the LCO Response Behaviors of the NATA modelChabalko, C. / Hajj, M. / Mook, D. / Silva, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3207
-
AIAA-2006-1853 Graphite Fiber Composites Reinforced With NanopaticlesHahn, H. / Kim, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3207
-
Graphite fiber composites reinforced with nanoparticlesKim, H.S. / Choi, O. / Hahn, H.T. et al. | 2006
- 3216
-
AIAA-2006-1854 (Student Paper) Fabrication and testing of long carbon nanontubes grown on the surface of fibers for hybrid compositesGarcia, E. / Hart, J. / Wardle, B. / Slocum, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3227
-
AIAA-2006-1855 Effect of the Localized Application of SWNT Modified Epoxy on the Interlaminar Shear Strength of Carbon Fiber LaminatesAdhikari, K. / Hubert, P. / Simard, B. / Johnston, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3237
-
AIAA-2006-1856 Flammability Properties and Microstructure Studies of Polymer NanocompositesKoo, J. / Pilato, L. / Wissler, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3256
-
Processing and characterization of epoxy/SWCNT/woven fabric compositesThakre, Piyush R. / Lagoudas, Dimitris C. / Zhu, Jiang / Barrera, Enrique V. / Gates, Thomas S. et al. | 2006
- 3256
-
AIAA-2006-1857 Processing and Characterization of Epoxy/SWCNT/Woven Fabric CompositesThakre, P. / Lagoudas, D. / Zhu, J. / Barrera, E. / Gates, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3267
-
Fabrication and characterization of carbon nanotube/glass fiber-reinforced multiscale compositesLiao, Yu-Hsuan / Liang, Zhiyong / Park, Young-Bin / Wang, Ben / Zhang, Chuck et al. | 2006
- 3267
-
AIAA-2006-1858 Fabrication and Characterization of Carbon Nanotube/Glass Fiber-Reinforced Multiscale CompositesLiao, Y. / Liang, Z. / Park, Y. / Wang, B. / Zhang, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3273
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Enhancement of the mechanical performance of carbon fiber reinforced epoxy resin composites by the introduction of carbon nano-fibers (CNF)Kostopoulos, Vassilis / Tsotra, Panayota / Karapappas, Petros / Vavouliotis, Antonios / Tsantzalis, Stavros / Friedrich, Klaus et al. | 2006
- 3273
-
AIAA-2006-1859 Enhancement of the Mechanical Performance of Carbon Fiber Reinforced Epoxy Resin Composites by the Introduction of Carbon Nano-Fibers (CNF)Kostopoulos, V. / Tsotra, P. / Karapappas, P. / Vavouliotis, A. / Tsantzalis, S. / Friedrich, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3283
-
AIAA-2006-1860 Global Control of Helicopter Vibrations Using a Semi-Active Vibration Control SystemHugin, C. / Hatch, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3291
-
AIAA-2006-1861 Vibration Reduction and Performance Enhancement in Rotorcraft Using Active Flaps at High Advance RatiosLiu, L. / Friedmann, P. / Kim, I. / Bernstein, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3310
-
AIAA-2006-1862 Nonlinear Flexible Multibody Dynamic Analysis of Rotor Blades with a Trailing Edge FlapDas, M. / Barut, A. / Madenci, E. / Straub, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3329
-
AIAA-2006-1865 Time and Frequency Domain Analysis of Whirl Flutter Stability in Tiltrotor AircraftsKim, T. / Shin, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3344
-
AIAA-2006-1866 Rotor Blade Dynamic Stall Model and Its Influence on Airfoil ResponseLaxman, V. / Venkatesan, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3365
-
AIAA-2006-1867 Joint Strike Fighter Airframe Durability and Damage Tolerance CertificationBall, D. / Norwood, D. / TerMaath, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3382
-
AIAA-2006-1868 Detail Part Optimization on the F-35 Joint Strike FighterTaylor, R. / Thomas, J. / Mackaron, N. / Riley, S. / Lajczok, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3396
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AIAA-2006-1869 Over the Failure, MLGSST for T-50 Supersonic Jet TrainerLee, B. / Kwak, D. / Park, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3403
-
AIAA-2006-1870 Structural Testing of an Ultralight UAV Composite WingSullivan, R. / Rais-Rohani, M. / Lacy, T. / Alday, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3413
-
AIAA-2006-1872 Modeling, Vibration and Instability of an Advanced Tiltrotor-Wing SystemSong, O. / Kwon, H. / Librescu, L. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3428
-
AIAA-2006-1874 A Rapid Stress Analysis Procedure for Generic Cutouts in Composite StructuresRussell, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3440
-
AIAA-2006-1875 Generating Curvilinear Fiber Paths from Lamination Parameters DistributionSetoodeh, S. / Blom, A. / Abdalla, M. / Gurdal, Z. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3440
-
Generating curvilinear fiber paths from lamination parameters distributionSetoodeh, Shahriar / Blom, Adriana W. / Abdalla, Mostafa M. / Gurdal, Zafer et al. | 2006
- 3453
-
Micromechanical analysis of composite truss-core sandwich panels for integral thermal protection systemsMartinez, Oscar / Bapanapalli, Satish / Sankar, Bhavani / Haftka, Raphael / Blosser, Max et al. | 2006
- 3453
-
AIAA-2006-1876 Micromechanical Analysis of Composite Truss-Core Sandwich Panels for Integral Thermal Protection SystemsMartinez, O. / Bapanapalli, S. / Sankar, B. / Haftka, R. / Blosser, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3472
-
Hybrid dynamic failure prediction tool for advanced composite structuresLua, Jim / Gregory, Bill / Gorfain, Josh / Daghei, Habib et al. | 2006
- 3472
-
AIAA-2006-1877 Hybrid Dynamic Failure Prediction Tool for Advanced Composite StructuresLua, J. / Gregory, B. / Gorfain, J. / Dagher, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3492
-
AIAA-2006-1878 Robust Bird-Strike Modeling Based on SPH Formulation Using LS-DYNAGoyal, V. / Huertas, C. / Leutwiler, T. / Borrero, J. / Vasko, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3509
-
AIAA-2006-1879 Coupled Acoustic and Heat Transfer Modeling of aSynthetic JetSeeley, C. / Arik, M. / Hedeen, R. / Wetzel, T. / Utturkar, Y. / Shih, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3522
-
AIAA-2006-1880 The Load-Deformation Analysis of Flanged Connection System Subjected to External LoadsZhang, Q. / Yang, G. / Sun, D. / Wang, L. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3532
-
AIAA-2006-1881 Development of an In-Flight Structural Health Monitoring System for Composite Unmanned AircraftKosmatka, J. / Oliver, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3543
-
AIAA-2006-1882 Nonlinear Structural Dynamics Characterization by Decomposing Time Signals Using Hilbert-Huang TransformPai, P. / Hu, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3561
-
AIAA-2006-1883 Application of the Random Decrement Technique to a Nonlinear Dynamic SystemShiryayev, O. / Slater, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3576
-
AIAA-2006-1884 Advanced System Interrogation Based on Active Bifurcation MorphingYin, S. / Epureanu, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3586
-
AIAA-2006-1885 Comparison of Inverse Structural Filter (ISF) and Sum of Weighted Accelerations (SWAT) Time Domain Force Identification MethodsAllen, M. / Carne, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3610
-
AIAA-2006-1886 Parameter Estimation of Spacecraft Fuel SloshSchlee, K. / Gangadharan, S. / Ristow, J. / Sudermann, J. / Walker, C. / Hubert, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3628
-
AIAA-2006-1887 Estimates of FRFs from Output-Only Data of a Space Mission Payload ComponentCoppotelli, G. / Crema, L. B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3640
-
AIAA-2006-1888 Actuation-Softening in Kagome Lattice StructuresLeung, A. / Guest, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3650
-
AIAA-2006-1891 Charge Determination for Specified Shape Coulomb Force Virtual StructuresParker, G. / King, L. / Schaub, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3658
-
AIAA-2006-1892 Development of an Integrated Aeroelastic Multi-Body Morphing Simulation ToolReich, G. / Bowman, J. / Sanders, B. / Frank, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3668
-
AIAA-2006-1893 Dynamic Modeling of Large-Scale Morphing AircraftSeigler, T. / Neal, D. / Inman, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3679
-
AIAA-2006-1895 Improved Composite Rigidization via Temperature-Controlled Resistive HeatingSarles, S. / Leo, D. / Riffle, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3679
-
Improved composite rigidization via temperature-controlled resistive heatingSarles, Stephen A. / Leo, Donald / Riffle, Judy et al. | 2006
- 3695
-
AIAA-2006-1896 Shape Memory Rigidizable Inflatable (RI) Structures for Large Space Systems ApplicationsLin, J. / Knoll, C. / Willey, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3695
-
Shape memory RI (rigidizable inflatable) structures for large space systems applicationsLin, John-K.H. / Knoll, Carl F. / Willey, Cliff E. et al. | 2006
- 3705
-
AIAA-2006-1897 Intelligent Flexible Materials for Deployable Space Structures (InFlex)Cadogan, D. / Scheir, C. / Dixit, A. / Ware, J. / Cooper, E. / Kopf, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3722
-
AIAA-2006-1898 New Deployable Membrane Structure Models Inspired by Morphological Changes in NatureKishimoto, N. / Natori, M. / Higuchi, K. / Ukegawa, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3726
-
AIAA-2006-1899 Thermo-Elastic Behaviour of Single Ply Triaxial Woven Fabric CompositesKueh, A. / Pellegrino, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3738
-
AIAA-2006-1900 Overview of Form Stiffened Thin Film Shell Characteristic BehaviorFlint, E. / Lindler, J. / Hall, J. / Rankine, C. / Regelbrugge, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3753
-
AIAA-2006-1901 Final Testing and Evaluation of a Meter-Class Actively Controlled Membrane MirrorPatrick, B. / Moore, J. / Chodimella, S. / Marker, D. / deBlonk, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3766
-
AIAA-2006-1902 Gore/Seam Cable Actuated Shape Control of Inflated Precision Gossamer Reflectors - Assessment StudyDeSmidt, H. / Wang, K. / Fang, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3779
-
AIAA-2006-1903 Experimental Validation of Discrete Location Boundary Shape Control for Thin Film ShellsFlint, E. / Lindler, J. / Hall, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3789
-
AIAA-2006-1904 Robustness of Thin Film Shells with Boundary ActuationLindler, J. / Flint, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3805
-
AIAA-2006-1905 Deployment Repeatability Testing of Composite Tape Springs for Space Optics ApplicationsBlack, J. / Whetzal, J. / deBlonk, B. / Massarello, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3819
-
AIAA-2006-1906 Reduced Order Models for Synthetic Jet Actuators on a Lifting Surface for Optimization and ControlSchober, S. / Marzocca, P. / De Breuker, R. / Abdalla, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3835
-
AIAA-2006-1907 Multi-Fidelity Gradient-Based Optimization in Turbomachinery Aerodynamic DesignJarrett, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3835
-
Multi-fidelity gradient-based optimization in turbomachinery aerodynamic designJarrett, Jerome P. et al. | 2006
- 3843
-
AIAA-2006-1908 Characterizing the Design Space in Multiobjective Axial Compressor Blade OptimizationMolinari, M. / Jarrett, J. / Clarkson, P. / Dawes, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3857
-
AIAA-2006-1909 Multidisciplinary Constraint Visualization and Trade-off Exploration in Aero Engine Preliminary DesignBell, T. / Jarrett, J. / Clarkson, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3868
-
AIAA-2006-1911 Global Design Optimization for Hypersonic Scramjet Propulsive FlowpathYu, W. X. / Bin, L. S. / Qian, C. X. / Guo, W. Z. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3878
-
AIAA-2006-1912 Integrated Transportation Network Design OptimizationTaylor, C. / de Weck, O. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3894
-
AIAA-2006-1913 A Framework for Aircraft Power Systems Optimizationvan Driel, E. / Slingerland, R. / Antoine, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3905
-
AIAA-2006-1914 NeuroDynamic Programming Approaches for Problems of Combined System-Design and Its Operational ManagementNusawardhana, A. / Crossley, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3918
-
AIAA-2006-1915 Optimizing the Optimization - A Method for Comparison of Optimization AlgorithmsOlvander, J. / Krus, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3930
-
AIAA-2006-1917 Implementation of Digital Pheromones for Use in Particle Swarm OptimizationFoo, J. / Kalivarapu, V. / Winer, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3943
-
AIAA-2006-1918 A Study of How the Nonlinearities of the Collapse Loading of Spherical Shells Can be Quantified in a Probabilistic FrameworkPepin, J. / Thacker, B. / Riha, D. / Pleming, J. / McKeighan, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3955
-
AIAA-2006-1919 Verification and Validation of a Penetration Model for the Design of a Blast Containment Vessel Part 1: Validation ExperimentsMullin, S. / Walker, J. / Riha, D. / Thacker, B. / Rodriguez, E. / Leslie, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3966
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AIAA-2006-1920 Verification and Validation of a Penetration Model for the Design of a Blast Containment Vessel Part II: Model ValidationRodriguez, E. / Pepin, J. / Riha, D. / Thacker, B. / Pleming, J. / Walker, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3977
-
AIAA-2006-1921 Development, Verification, and Validation of a Parametric Cervical Spine Injury Prediction ModelNicolella, D. / Francis, W. / Bonivtch, A. / Thacker, B. / Paskoff, G. / Shender, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 3986
-
AIAA-2006-1922 Validation of Uncertainty Quantification for Structures with Encapsulated Epoxy FoamHasselman, T. / Lloyd, G. / Hinnerichs, T. / O Gorman, C. / Urbina, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4001
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AIAA-2006-1923 Uncertainty Quantification During Integral Validation: Estimating Parametric, Model Form, and Solution ContributionsLogan, R. / Nitta, C. / Chidester, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4007
-
AIAA-2006-1924 Nonlinear Random Response of a Clamped Plate: A Well-Characterized ExperimentGordon, R. / Hollkamp, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4025
-
AIAA-2006-1926 Reduced-Order Modeling of Random Response of Curved Beams Using Implicit CondensationGordon, R. / Hollkamp, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4036
-
AIAA-2006-1927 Response of Plates Under Uniform Random Loads Unsynchronized in TimeDhainaut, J. / Cheng, G. / Mei, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4047
-
AIAA-2006-1928 The Nonlinear Response of a Plate to Acoustic Loading: Predictions and ExperimentsHollkamp, J. / Beberniss, T. / Gordon, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4064
-
AIAA-2006-1929 Using Load-based Ritz Vectors for Dynamic Analysis of StructuresRose, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4074
-
AIAA-2006-1931 Computational Dynamics in Design OptimizationVanderplaats, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4083
-
AIAA-2006-1933 Frequency Response Analysis of Complex Structures: Issues, Trends, and Recent DevelopmentsBenninghof, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4091
-
AIAA-2006-1934 Modeling of Aeroservoelastic Systems with Nonlinear Strain ActuationMoulin, B. / Karpel, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4100
-
AIAA-2006-1935 Development of Aeroservoelastic Analytical Models and Gust Load Alleviation Control Laws of a SensorCraft Wind-Tunnel Model Using Measured DataSilva, W. / Vartio, E. / Shimko, A. / Kvaternik, R. / Eure, K. / Scott, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4117
-
AIAA-2006-1936 Reduced-Size Aeroservoelastic Modeling and LCO Simulations with Structurally Non-Linear ActuatorsGold, P. / Karpel, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4128
-
AIAA-2006-1937 Aeroservoelasticity Interactions Studies on a Business AircraftBotez, R. / Dinu, A. / Cotoi, I. / Stathopoulos, N. / Dickinson, M. / Therien, S. / Rathe, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4138
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AIAA-2006-1938 Characterization of Methods for Computation of Aeroservoelastic Systems Response to Gust ExcitationAzoulay, D. / Karpel, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4153
-
AIAA-2006-1939 Aeroelastic Response and Active Control of Aircraft Wings Modeled as Thin-Walled BeamsLibrescu, L. / Qin, Z. / Na, S. / Yoon, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4170
-
AIAA-2006-1940 Path Definitions for Elastically Tailored Conical ShellsBlom, A. / Tatting, B. / Hol, J. / Gurdal, Z. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4184
-
Reliability based design optimization of cantilever beams under fatigue constraintHonarmandi, Peyman / Zu, Jean-W. / Behdinan, Kamran et al. | 2006
- 4184
-
AIAA-2006-1941 Reliability Based Design Optimization of Cantilever Beams Under Fatigue ConstraintHonarmandi, P. / Zu, J. / Behdinan, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4197
-
AIAA-2006-1942 Analysis and Design of Corrugated-Core Sandwich Panels for Thermal Protection Systems of Space VehiclesBapanapalli, S. / Martinez, O. / Gogu, C. / Sankar, B. / Haftka, R. / Blosser, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4215
-
AIAA-2006-1943 Difficulties in Optimization of Imperfect Stiffened Cylindrical ShellsBushnell, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4339
-
AIAA-2006-1944 Tailoring Static Strength Performance of Metallic Stiffened Panels by Selective Local Sub-StiffeningMurphy, A. / Quinn, D. / Mawhinney, P. / Ozakca, M. / van der Veen, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4355
-
AIAA-2006-1945 Truss Beam with Tendon Diagonals --- Mechanics and DesignsGreschik, G. / Michii, Y. / Palisoc, A. / Derbes, B. / Veal, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4371
-
AIAA-2006-1946 Self-Healing Polymers for Space ApplicationsChipara, M. / Zaleski, J. / Dragnea, B. / Shansky, E. / Onuta, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4380
-
AIAA-2006-1948 Multifunctional Carbon Nanocomposite Coatings for Space StructuresRawal, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4387
-
AIAA-2006-1950 Constitutive Modeling of Multi-Functional Energetic Structural Materials: Plasticity EffectsReding, D. / Lu, X. / Narayanan, V. / Hanagud, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4396
-
Novel shape memory of metal nanowires through reversible lattice reorientationsLiang, Wuwei / Zhou, Min et al. | 2006
- 4396
-
AIAA-2006-1951 Novel Shape Memory of Metal Nanowires Through Reversible Lattice ReorientationsLiang, W. / Zhou, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4407
-
The role of structural health monitoring for future air vehiclesDerriso, Mark M. / Olson, Steven E. et al. | 2006
- 4407
-
AIAA-2006-1952 The Role of Structural Health Monitoring for Future Air VehiclesDerriso, M. / Olson, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4415
-
AIAA-2006-1955 Damage Detection of Low Energy Impacts in a Composite UAV WingTrickey, S. / Nichols, J. / Seaver, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4425
-
AIAA-2006-1956 Hybrid Sensor Network for Large Array Sensing Systems for Acoustic Source Localization in Solid MediaGhoshal, A. / Kim, H. / Chattopadhyay, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4437
-
AIAA-2006-1957 Spectral Finite Element Modeling of Complex Structures for Applications in Real-time Structural Health MonitoringMahapatra, D. R. / Gopalakrishnan, S. / Hu, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4444
-
Co-bonded composite joints using Z-fiber(trademark) stubbleClay, Stephen B. / Pommer, Amanda K. et al. | 2006
- 4444
-
AIAA-2006-1958 Co-Bonded Composite Joints Using Through Thickness Z-Fiber(TM) StubbleClay, S. / Pommer, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4455
-
AIAA-2006-1959 Dimensionless parameters in symmetric double lap joints: an orthotropic solution for thermomechanical loadingGustafson, P. / Bizard, A. / Waas, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4472
-
AIAA-2006-1960 Analytical and Numerical Results for an Adhesively Bonded Joint Subjected to Pure BendingSmeltzer, S. / Lundgren, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4484
-
AIAA-2006-1961 Dynamic Fracture Analysis of Adhesively Bonded Joints Using Explicit MethodsMakhecha, D. / Kapania, R. / Johnson, E. / Dillard, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4484
-
Dynamic fracture analysis of adhesively bonded joints using explicit methodsMakhecha, Dhaval P. / Kapania, Rakesh K. / Johnson, Eric R. / Dillard, David A. et al. | 2006
- 4499
-
Failure analysis of adhesively bonded composite joints via the virtual crack closure techniqueYarrington, Phillip W. / Collier, Craig S. / Bednarcyk, Brett A. et al. | 2006
- 4499
-
AIAA-2006-1962 Failure Analysis of Adhesively Bonded Composite Joints via the Virtual Crack Closure TechniqueYarrington, P. / Collier, C. / Bednarcyk, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4514
-
AIAA-2006-1963 Thermo-Mechanical Analysis of Bonded Cylindrically Curved Composite Shell StructuresOterkus, E. / Madenci, E. / Smeltzer, S. / Ambur, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4514
-
Thermo-mechanical analysis of bonded cylindrically curved composite shell structuresOterkus, E. / Madenci, E. / Smeltzer III, S.S. / Ambur, D.R. et al. | 2006
- 4540
-
AIAA-2006-1964 Experimental Monte Carlo Mistuning Assessment of Bladed Disk Vibration Using Forcing VariationsLi, J. / Castanier, M. / Pierre, C. / Ceccio, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4540
-
Experimental Monte Carlo mistuning assessment of bladed disk vibration using forcing variationsLi, Jia / Castanier, Matthew P. / Pierre, Christophe / Ceccio, Steven L. et al. | 2006
- 4549
-
AIAA-2006-1965 Modeling Cylinder Flow Vortex Shedding with Enforced Motion Using a Harmonic Balance ApproachSpiker, M. / Thomas, J. / Hall, K. / Kielb, R. / Dowell, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4549
-
Modeling cylinder flow vortex shedding with enforced motion using a harmonic balance approachSpiker, Meredith A. / Thomas, Jeffrey P. / Hall, Kenneth C. / Kielb, Robert E. / Dowell, Earl H. et al. | 2006
- 4559
-
AIAA-2006-1966 A Resonant Synchronous Vibration Based Approach for Rotor Imbalance DetectionLuo, H. / Rodriguez, H. / Hallman, D. / Lewicki, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4579
-
AIAA-2006-1968 Aeroelastic Analysis of an Isolated Airfoil Under a Pulsating FlowCho, S. / Kim, T. / Song, S. / Shin, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4590
-
Some factors affecting the shape recovery properties of NiTi SMAWada, Kiyohide / Liu, Yong et al. | 2006
- 4590
-
AIAA-2006-1969 Some factors affecting the shape recovery properties of NiTi SMAWada, K. / Liu, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4607
-
AIAA-2006-1972 The application of residual stress tailoring of snap-through composites for variable sweep wingsMattioni, F. / Gatto, A. / Weaver, P. / Friswell, M. / Potter, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4619
-
AIAA-2006-1973 Loss in Coupling Due to Crack in Piezoelectric Wafer Based Sensors and ActuatorsZhou, X. / Chattopadhyay, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4619
-
Loss in coupling due to crack in piezoelectric wafer based sensors and actuatorsZhou, Xu / Chattopadhyay, Aditi et al. | 2006
- 4631
-
AIAA-2006-1975 Enhancing The Effective Bandwidth of A Membrane Optic Using A Shallow, Fluid-Filled CavityRuggiero, E. / Inman, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4645
-
AIAA-2006-1976 Control of a Space Rigidizable-Inflatable Boom Using Embedded Piezoelectric Composite ActuatorsTarazaga, P. / Inman, D. / Wilkie, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4659
-
AIAA-2006-1977 Modal identification for modeling a deployed tape-springhexapodAridon, G. / Blanchard, L. / Remond, D. / Dufour, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4667
-
AIAA-2006-1978 Active Vibration Suppression Strategy for a Membrane Reflector/Mirror Undergoing Slewing ManeuversSakamoto, H. / Park, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4687
-
AIAA-2006-1979 Minimum Angular-Impulse Control for ISATCliff, E. / Herdman, T. / Liu, Z. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4711
-
AIAA-2006-1980 Dynamic Properties of Rotationally Skew Fold Membrane for Spinning Solar SailFuruya, H. / Inoue, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4722
-
AIAA-2006-1981 Rapid Generation and Assessment of Aircraft Structural Topologies for Multidisciplinary Optimization and Weight EstimationSensmeier, M. / Stewart, B. / Samareh, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4734
-
AIAA-2006-1982 Topology Optimization of a Curved Thermal Protection SystemPrithivirajan, M. / Haney, M. / Grandhi, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4757
-
AIAA-2006-1983 Structural Topology Optimization Based On Virtual Testing With General ConstraintsBelegundu, A. / Rajan, S. / Wuppalapati, S. / Nandakwang, P. / Gianforcaro, R. / StVille, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4767
-
AIAA-2006-1984 Investigation on the Validity of Topology Optimisation MethodsEdwards, C. / Kim, H. / Budd, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4782
-
AIAA-2006-1986 Structural Topology Optimization Using Two-Level Dynamic Condensation SchemePark, S. / Kim, H. / Cho, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4801
-
AIAA-2006-1987 Fault Detection with Uncertain PriorsBen-Haim, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4805
-
AIAA-2006-1988 Sensitivity Analysis of Stochastic SystemsSarkar, A. / Ghanem, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4810
-
AIAA-2006-1989 Some Issues and Needs in Quantification of Margins and Uncertainty (QMU) in Complex Coupled SystemsRomero, V. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4832
-
AIAA-2006-1990 Component-Mode-Based Monte Carlo Simulation for Efficient Probabilistic Vibration AnalysisLee, S. / Castanier, M. / Pierre, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4832
-
Component-mode-based Monte Carlo simulation for efficient probabilistic vibration analysisLee, Soo-Yeol / Castanier, Matthew P. / Pierre, Christophe et al. | 2006
- 4845
-
AIAA-2006-1991 Novel Stochastic Concepts And Algorithms Integrated Within A Graphically-Assisted Reliability Prediction System For Aircraft Jet Engine Rotating AssemGhiocel, D. / Wang, L. / An, N. / Thorpe, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4845
-
Novel stochastic concepts and algorithms integrated within a graphically-assisted reliability prediction system for aircraft jet engine rotating assembliesGhiocel, Dan M. / An, Ning / Wang, Letian / Thorpe, Phil et al. | 2006
- 4854
-
AIAA-2006-1992 Development of Factors of Safety for Structural Analysis and Verification of Cryogenic Structures Using Probabilistic MethodsHerbert, J. / Trilling, L. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4867
-
AIAA-2006-1993 Convergence Studies of Wiener Expansions for Computational Nonlinear MechanicsPettit, C. / Beran, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4885
-
AIAA-2006-1994 Verification of Stochastic Solutions Using Polynomial Chaos ExpansionsHuyse, L. / Bonivtch, A. / Pleming, J. / Riha, D. / Waldhart, C. / Thacker, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4894
-
AIAA-2006-1995 Non-Linear Error Ansatz Models in Space and Time for Solution VerificationHemez, F. / Brock, J. / Kamm, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4909
-
AIAA-2006-1996 Towards a validated system model: assessment of fixed joint uncertaintyRutherford, A. / Pepin, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4917
-
AIAA-2006-1997 Statistical Methods for Model Validation under UncertaintyRebba, R. / Mahadevan, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4927
-
AIAA-2006-1998 A Practical Look at the Massively Parallel FEA Code SalinasRohl, P. / Reese, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4936
-
AIAA-2006-1999 Integration of Shell FEA with Geometric Modeling on NURBS Surface Representation for Practical ApplicationsCho, M. / Choi, J. / Roh, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4954
-
AIAA-2006-2001 Impact of Uncertainty Quantification on Design Decisions for a Hydraulic-Hybrid Powertrain EngineKokkolaras, M. / Mourelatos, Z. / Papalambros, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4954
-
Impact of uncertainty quantification on design decisions for a hydraulic-hybrid powertrain engineKokkolaras, Michael / Mourelatos, Zissimos P. / Papalambros, Panos Y. et al. | 2006
- 4964
-
AIAA-2006-2002 Reliability-Based Topology Optimization of Frame Structure with Multiple ModesKogiso, N. / Mogami, K. / Nishiwaki, S. / Izui, K. / Yoshimura, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4976
-
AIAA-2006-2003 Stochastic Finite Element Failure Analysis of Laminated Plates Under Uniaxial Compressive LoadingOnkar, A. / Upadhyay, C. / Yadav, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 4990
-
AIAA-2006-2004 An Experimental and Numerical Study of Compression-Loaded Composite Panels with CutoutsThornburgh, R. / Hilburger, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5018
-
AIAA-2006-2005 A Statistics Based Method for Mapping Flight Strains to LoadsPadmanabhan, M. / Nagesh, K. / Elattuvalappil, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5028
-
Thermomechanical behavior and experimental testing of flexible matrix composite box-beams with extension-twist couplingNampy, Sreenivas N. / Smith, Edward C. et al. | 2006
- 5028
-
AIAA-2006-2006 Thermomechanical Behavior and Experimental Testing of Flexible Matrix Composite Box-Beams with Extension-Twist couplingNarayanan-Nampy, S. / Smith, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5043
-
AIAA-2006-2007 Thermal Deformation Measurement of Onboard Antenna Reflector in Thermal Vacuum Chamber by PhotogrammetryOzawa, S. / Fukatsu, A. / Shimizu, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5052
-
AIAA-2006-2008 Transient Response of Composite Sandwich Panels Subjected to Blast Wave PressureCelik, E. / Guven, I. / Madenci, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5062
-
AIAA-2006-2009 Crack Tip Fields in Functionally Graded Materials with Temperature-Dependent PropertiesJin, Z. / Batra, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5066
-
AIAA-2006-2010 Exact Plane-Strain Solutions for Functionally Graded Multilayered Isotropic Cylinders under Static DeformationPan, E. / Roy, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5076
-
AIAA-2006-2011 Nonlinear Static Analysis of a Beam Made of Functionally Graded MaterialDeschilder, M. / Eslami, H. / Zhao, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5085
-
AIAA-2006-2012 Propagation of Damage in Functionally Graded Materials Under Impact LoadsThamburaj, P. / Johnson, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5092
-
AIAA-2006-2015 Permeability of Polymer Composites for Cryogenic ApplicationsBechel, V. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5092
-
Permeability of polymer composites for cryogenic applicationsBechel, Vernon T. / Arnold, Fred et al. | 2006
- 5103
-
AIAA-2006-2016 An Experimental Investigation of the Effect of Thermal Shock on Damage in Cryogenic Composite LaminatesOh, B. / Kawatsuji, Y. / Kinra, V. / Lagoudas, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5111
-
AIAA-2006-2017 Hydrogen Gas Leak Rate Testing and Post-Testing Assessment of Microcrack Damaged Composite LaminatesGrenoble, R. / Gates, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5111
-
Hydrogen gas leak rate testing and post-testing assessment of microcrack damaged composite laminatesGrenoble, Ray W. / Gates, Thomas S. et al. | 2006
- 5121
-
AIAA-2006-2018 Determination of Allowable Hydrogen Permeation Rates in Launch Vehicle Propellant TanksRobinson, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5132
-
AIAA-2006-2020 Fracture Toughness of Space Shuttle External Tank Insulation FoamGanpatye, A. / Kinra, V. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5139
-
AIAA-2006-2021 A Reduced Damping Model Derived from CFD Based Aeroelastic SimulationsBadcock, K. / Woodgate, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5158
-
AIAA-2006-2022 CFD-Based Discrete Gust Response Analysis of Elastic WingsRaveh, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5176
-
AIAA-2006-2023 Application of Higher-Order Harmonic Balance to Non-Linear Aeroelastic SystemsDimitriadis, G. / Amuyedo, N. / Vio, G. / Cooper, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5188
-
AIAA-2006-2024 Nonlinear Aeroelastic Analysis Using a CFD-Based State Space ROMMunteanu, S. / Rajadas, J. / Chattopadhyay, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5207
-
AIAA-2006-2025 Unified Rational Function Approximation Formulation for Aeroelastic and Flight Dynamic AnalysisBaldelli, D. / Chen, P. / Panza, J. / Adams, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5229
-
AIAA-2006-2026 Flutter Simulation and Prediction with CFD-Based Reduced-Order ModelLai, K. / Won, K. / Koh, E. / Tsai, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5246
-
AIAA-2006-2027 Shear Post-Buckling Behaviour of Glare Modelling Fiberglass DamegeAiroldi, A. / Lanzi, L. / Sala, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5246
-
Shear post-buckling behavior of Glare modeling fiberglass damageAiroldi, A. / Lanzi, L. / Sala, G. et al. | 2006
- 5263
-
AIAA-2006-2028 The Incorrect Benchmark Shell Buckling SolutionWardle, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5274
-
AIAA-2006-2029 Improved Reliability of Buckling Load Calculations Using Multi-Level High-Fidelity AnalysisHol, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5287
-
AIAA-2006-2030 On the Accuracy of Buckling Calculations Using Smeared StiffenersArbocz, J. / Hol, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5292
-
AIAA-2006-2031 Physical Insight into the Buckling Phenomena of Composite StructuresWeaver, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5301
-
AIAA-2006-2032 Unified Procedure for Structural and Parameteric Identification of Nonlinear Aeroelastic and Aeroservoelastic SystemsMoulin, B. / Baldelli, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5308
-
AIAA-2006-2033 Statistical Analysis Tools for Detection of Non-Linearity in Aeroelastic PhenomenaPopescu, C. / Wong, Y. / Lee, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5321
-
AIAA-2006-2034 Identification of Nonlinear Aeroelastic and Aeroservoelastic Systems Using High-Order Iterative TechniqueMoulin, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5337
-
AIAA-2006-2035 SHARCS Project: Modal Parameters Identification of Smart Spring/Helicopter Blade SystemCoppotelli, G. / Marzocca, P. / Ulker, F. / Campbell, J. / Nitzsche, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5349
-
AIAA-2006-2036 Effects of Proper Orthogonal Decomposition on Identification Using the Minimum Model Error AlgorithmShiryayev, O. / Slater, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5361
-
AIAA-2006-2037 Non-Linear System Identification of Theoretical and Experimental Data for Mechanical SystemsVio, G. / Dimitriadis, G. / Shi, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5374
-
AIAA-2006-2038 Veritex(TM) Struts for Antenna ApplicationsSchueler, R. / Pora, E. / Traxler, E. / Hermiller, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5379
-
AIAA-2006-2039 Qualification of Elastic Memory Composite Hinges for Spaceflight ApplicationsBarrett, R. / Lake, M. / Francis, W. / Abrahamson, E. / Scherbarth, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5389
-
AIAA-2006-2040 Nonlinear Modeling and Control Design of Active Helicopter BladesAlthoff, M. / Patil, M. / Traugott, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5389
-
Nonlinear modeling and control design of active helicopter bladesAlthoff, Matthias / Patil, Mayuresh J. / Traugott, Johannes P. et al. | 2006
- 5407
-
AIAA-2006-2041 Morphing Airfoil Design for Minimum Aerodynamic Drag and Actuation Energy Including Aerodynamic WorkNamgoong, H. / Crossley, W. / Lyrintzis, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5422
-
AIAA-2006-2042 Developing Morphing Wing Weight Predictors with Emphasis on the Actuating MechanismSkillen, M. / Crossley, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5439
-
AIAA-2006-2043 Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber ModelRicci, S. / Scotti, A. / Terraneo, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5451
-
AIAA-2006-2044 Genetic Algorithm Approach to Adaptive Tuning of Acoustic Control on a Launch VehicleWhitaker, G. / Griffin, S. / Farinholt, K. / Skinner, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5462
-
AIAA-2006-2045 A New Selection-Integrated Optimization (SIO) Methodology for Adaptive Systems OptimizationKhire, R. / Messac, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5479
-
AIAA-2006-2046 Mixed-Discrete Multiobjective Optimization of Fuzzy SystemsRao, S. / Xiong, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5523
-
AIAA-2006-2047 Multi-Objective Genetic Algorithm Concurrent Subspace Optimization (MOGACSSO) for Multidisciplinary DesignParashar, S. / Bloebaum, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5534
-
Life cycle cost based economic assessment of Active Building Envelope (ABE) systemsRivas, Flor / Khire, Ritesh A. / Messac, Achille / Van Dessel, Steven et al. | 2006
- 5534
-
AIAA-2006-2048 Life Cycle Cost Based Economic Assessment of Active Building Envelope (ABE) SystemsRivas, F. / Khire, R. / Messac, A. / Van Dessel, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5549
-
AIAA-2006-2049 Rapid Optimization-Based Conceptualization of Multiple-Bend Spring ConceptsMattson, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5558
-
AIAA-2006-2050 Surrogate Assisted Evolutionary Algorithm for Multiobjective OptimizationRay, T. / Smith, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5566
-
AIAA-2006-2052 An Evaluation of Some Alternative Formulations for Transient Dynamic Response OptimizationWang, Q. / Arora, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5579
-
AIAA-2006-2054 Shape Sensitivities of Thermoelastic Structures with Internal and External RadiationBhatia, M. / Livne, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5604
-
AIAA-2006-2056 Multilevel Crashworthiness Design using a Compliant Mechanism ApproachPatel, N. / Kang, B. / Renaud, J. / Tovar, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5618
-
AIAA-2006-2058 System Design of Missile Based on CO with Variable Complexity ModelingLin, X. / Yu, W. X. / Li, Y. / Qian, C. X. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5625
-
AIAA-2006-2059 Reliability Based Aircraft Structural Design Pays Even with Limited Statistical DataAcar, E. / Haftka, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5644
-
AIAA-2006-2062 A Non-Deterministic Aircraft Sizing Method Under Probabilistic Design ConstraintsNam, T. / Soban, D. / Mavris, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5659
-
AIAA-2006-2064 Reliability Based Optimization Approach for Nondestructive Inspection PlanningKuntiyawichai, K. / Schueller, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5659
-
Reliability based optimization approach for nondestructive inspection planningSchueller, G.I. / Kuntiyawichai, K. et al. | 2006
- 5672
-
AIAA-2006-2065 Calculation Verification: Pointwise Estimation of Solutions and Their Method-Associated Numerical ErrorSmitherman, D. / Kamm, J. / Brock, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5687
-
AIAA-2006-2066 Using Polynomial Chaos for Uncertainty Quantification in Problems with NonlinearitiesWitteveen, J. / Bijl, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5705
-
AIAA-2006-2068 Stochastic Eigenvalue Problem with Polynomial ChaosMulani, S. / Kapania, R. / Walters, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5729
-
AIAA-2006-2070 Domain Decomposition of Stochastic SystemsSarkar, A. / Ghanem, R. / Benabbou, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5737
-
AIAA-2006-2071 An Efficient Monomial Chaos Approach for Uncertainty Quantification in Nonlinear Computational ModelsWitteveen, J. / Bijl, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5754
-
AIAA-2006-2072 Non-Probabilistic Uncertainty Assessment in Finite Element Models with SuperelementsDe Gersem, H. / Moens, D. / Desmet, W. / Vandepitte, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5772
-
AIAA-2006-2073 Parallel Algorithm for Fully Nonlinear Aeroelastic AnalysisGargoloff, J. / Cizmas, P. / Strganac, T. / Beran, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5783
-
AIAA-2006-2075 Numerical Simulation of the Buffet of a Full Span Delta Wing at High Angle of AttackAttar, P. / Gordnier, R. / Visbal, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5806
-
AIAA-2006-2076 Comparative Analysis of Computational Methods for Limit-Cycle OscillationsGopinath, A. / Beran, P. / Jameson, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5818
-
AIAA-2006-2077 Treatment of Complex Configurations for Flutter CalculationsRampurawala, A. / Badcock, K. / Woodgate, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5841
-
AIAA-2006-2079 Transonic Flutter Prediction of Supersonic Jet Trainer with Various External Store ConfigurationsLee, I. / Kwon, H. / Kim, J. / Yoo, J. / Paek, S. / Kim, Y. / Bae, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5848
-
AIAA-2006-2080 Design of a Roll Out and Passively Deployed Solar ArrayCampbell, D. / Barrett, R. / Lake, M. / Francis, W. / Keller, P. / Scherbarth, M. / Freebury, G. / Beidleman, N. / Abbott, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5856
-
AIAA-2006-2082 Structural Configuration Analysis of Crew Exploration Vehicle ConceptsMukhopadhyay, V. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5864
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AIAA-2006-2083 Design Exploration for a Modular Optical Space Telescope Architecture Using Parameterized Integrated ModelsUebelhart, S. / Cohan, L. / Miller, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5876
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AIAA-2006-2084 Analysis Driven Design and Optimization Methods for Aircraft StructuresMoore, R. / Murphy, A. / Price, M. / Curran, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5894
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AIAA-2006-2086 Further Refinement of Material Models for Hypervelocity Gouging ImpactsCinnamon, J. / Palazotto, A. / Brar, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5910
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AIAA-2006-2087 Further Investigation of a Scaled Hypervelocity Gouging Model and Validation of Material Constitutive ModelsCinnamon, J. / Palazotto, A. / Szmerekovsky, A. / Pendleton, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5924
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AIAA-2006-2088 Adiabatic Shear Banding for Different Metals at High Velocity ImpactVoyiadjis, G. / Abed, F. / Palazotto, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5928
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AIAA-2006-2089 Modeling and Simulation of Perforation of Steel Plates by Blunt ProjectilesVoyiadjis, G. / Al-Rub, R. A. / Palazotto, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5932
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AIAA-2006-2090 An Improved Study of Temperature Changes During Hypervelocity Sliding High Energy ImpactSzmerekovsky, A. / Palazotto, A. / Cinnamon, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5942
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AIAA-2006-2092 Composites Containing Barrier Layers for Reduced Permeability at Cryogenic TemperaturesKim, R. / Bechel, V. / Donaldson, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5942
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Composites containing barrier layers for reduced permeability at cryogenic temperatureBechel, Vernon T. / Kim, Ran-Y. / Donaldson, Steven L. et al. | 2006
- 5953
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AIAA-2006-2093 Parametric Investigation of Gas Permeability in Cross-Ply Composite Laminates Using Three-Dimensional Finite ElementsXu, J. / Sankar, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5953
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Parametric investigation of gas permeability in cross-ply composite laminates using three-dimensional finite elementsXu, Jianlong / Sankar, Bhavani V. et al. | 2006
- 5965
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Modeling of permeability in composite laminates with delaminations and stitch cracksRoy, Samit / Nair, Abilash et al. | 2006
- 5965
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AIAA-2006-2094 Modeling of Permeability in Composite Laminates with Delaminations and Stitch CracksRoy, S. / Nair, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5982
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AIAA-2006-2097 The Effect of the Microstructure on the Stiffness and Strength of Closed Cell FoamsSue, J. / Whitcomb, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 5982
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The effect of the microstructure on the stiffness and strength of closed cell foamsJiwoong, Sue / Whitcomb, John et al. | 2006
- 5996
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Effect of inclusion morphology on the coefficient of thermal expansion of a filled polymer matrixMallick, Kaushik / Cronin, John / Arzberger, Steven et al. | 2006
- 5996
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AIAA-2006-2098 Effect of Inclusion Morphology on the Coefficient of Thermal Expansion in Filled Epoxy MatrixMallick, K. / Cronin, J. / Arzberger, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 6007
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AIAA-2006-2100 Buckling of Curved Shells with Free Edges Under Multi-Axis LoadingSilver, M. / Hinkle, J. / Peterson, L. / Warren, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 6038
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AIAA-2006-2101 Natural Frequencies of an Innovative Space Based Radar Antenna by Continuum ModelingSalehian, A. / Inman, D. / Cliff, E. / American Institute of Aeronautics and Astronautics et al. | 2006