| 61 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Aerodynamics of Gurney Flaps on a Wing in Ground Effect/
|
Zerihan, J
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 62 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Characterization and Analysis of Magnetorheological Damper Behavior Under Sinusoidal Loading/
|
Snyder, R A
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 63 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Compressible Dynamic Stall Control Using Dynamic Shape Adaptation (TN)/
|
Chandrasekhara, M S
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 64 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Computational Aeroacoustic Analysis of Slat Trailing-Edge Flow/
|
Singer, B A
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 65 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Computation of Mistuning Effects on Cascade Flutter/
|
Sadeghi, M
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 66 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Convergence Acceleration of an Inverse Design Technique for Constructing Turbomachinery Cascades (TN)/
|
Yokota, J W
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 67 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Coupled Analytical Sensitivity Analysis and Optimization of Three-Dimensional Nonlinear Aeroelastic Systems/
|
Maute, K
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 68 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Coupled Helicopter Rotor/Flexible Fuselage Aeroelastic Model for Control of Structural Response/
|
Cribbs, R C
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 69 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Damping Perturbation Method for Flutter Solution: The g-Method/
|
Chen, P C
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 70 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Detection and Repair of Poorly Converged Optimization Runs/
|
Kim, H
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 71 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Diffusion Timescale of Porous Pressure-Sensitive Paint (TN)/
|
Liu, T
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 72 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Double Flutter in an Aeroelastic System (TN)/
|
Chamara, R A
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 73 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Effect of Ribs on Suddenly Expanded Flows (TN)/
|
Rathakrishnan, E
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 74 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Effect of Wall Shear Stress on Structural Vibration (TN)/
|
Frendi, A
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 75 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Effects of Angle of Attack on Nonlinear Flutter of a Delta Wing/
|
Tang, D
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 76 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Effects of Wall Admittance Changes on Aeroelastic Stability of Turbomachines/
|
Sun, X
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 77 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Elastic-Dynamic Rotor Blade Design with Multiobjective Optimization/
|
Kim, J-E
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 78 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Euler-Based Inverse Method for Turbomachine Blades, Part 2: Three-Dimensional Flows/
|
Dang, T
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 79 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Evaluation of Damage Tolerance Analysis Tools for Lap Joints/
|
Trego, A
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 80 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Experimental Investigation of Two-Stream Mixing Flow with Multiple Tabs/
|
Yu, S C M
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
