| 81 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Theoretical Model for Airfoils to Suppress Leading-Edge Separation/
|
Yeung, W W H
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 82 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Theory for Conical Membrane Wings of High Aspect Ratio/
|
Jackson, P S
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
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|
| 83 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Thermal Buckling of Axially Precompressed Cylindrical Shells Irradiated by Laser Beam/
|
Keshun, D
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 84 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Unsteady Flow Calculations with a Parallel Multiblock Moving Mesh Algorithm/
|
Tsai, H M
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
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|
| 85 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Unsteady Forces on a Two-Dimensional Wing in Plunging and Pitching Motions/
|
Sunada, S
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
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| 86 |
|
Airfoil Boundary-Layer Development and Transition with Large Leading-Edge Roughness
|
Kerho, M. F
|
American Institute of Aeronautics and Astronautics
|
1997
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|
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| 87 |
|
Airfoil Flow Visualization and Pressure Measurements in High-Reynolds-Number Transonic Flow/
|
Olivier, H
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
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|
| 88 |
|
Airfoil Theory for Non-Uniform Motion/
|
von Karman, T
|
American Institute of Aeronautics and Astronautics
|
1900
|
|
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|
| 89 |
|
Algebraic Turbulence Modeling for Swept Shock-Wave/Turbulent Boundary-Layer Interactions
|
Panaras, A. G
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 90 |
|
Algebraic Turbulence Model Simulations of Supersonic Open-Cavity Flow Physics
|
Tam, C.-J
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
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| 91 |
|
Alternative Control Logic for Type-II Variable-Stiffness-System (TN)
|
Onoda, J
|
American Institute of Aeronautics and Astronautics
|
1996
|
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| 92 |
|
Analysis and Experiment of Gas Leakage Through Composite Laminates for Propellant Tanks/
|
Kumazawa, H
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
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| 93 |
|
Analysis of Compressible Light Dynamic Stall Flow at Transitional Reynolds Numbers
|
Van Dyken, R. D
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
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|
| 94 |
|
Analysis of Cracked Aluminum Plates Repaired with Bonded Composite Patches
|
Sun, C. T
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
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|
| 95 |
|
Analysis of Flow Conditions in Freejet Experiments for Studying Airfoil Self-Noise/
|
Moreau, S
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
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|
| 96 |
|
Analysis of Nonlinear Aeroelastic Signals/
|
Alighanbari, H
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 97 |
|
Analysis of Piezoelastic Structures with Laminated Piezoelectric Triangle Shell Elements
|
Tzou, H. S
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 98 |
|
Analysis of Sandwich Plates with Viscoelastic Damping Using Two-Dimensional Plate Modes/
|
Wang, G
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
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|
| 99 |
|
Analysis of Streamline Curvature Effects on Wall-Bounded Turbulent Flows
|
Luo, J
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
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|
| 100 |
|
Analysis of Subgrid-Scale Torque for Large-Eddy Simulation of Turbulence/
|
Marshall, J. S
|
American Institute of Aeronautics and Astronautics
|
2003
|
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