| 61 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Effects of Wall Admittance Changes on Aeroelastic Stability of Turbomachines/
|
Sun, X
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 62 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Elastic-Dynamic Rotor Blade Design with Multiobjective Optimization/
|
Kim, J-E
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 63 |
|
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
|
|
|
|
| 64 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Evaluation of Damage Tolerance Analysis Tools for Lap Joints/
|
Trego, A
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 65 |
|
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
|
|
|
|
| 66 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Kriging Models for Global Approximation in Simulation-Based Multidisciplinary Design Optimization/
|
Simpson, T W
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 67 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Modeling the Shapes of Constrained Partially Inflated High-Altitude Balloons/
|
Baginski, F
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 68 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Nonlinear Response of Airfoil Section with Control Surface Freeplay to Gust Loads/
|
Tang, D
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 69 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Nonlinear Response of Composite Panels Under Combined Acoustic Excitation and Aerodynamic Pressure/
|
Abdel-Motagaly, K
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 70 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Nonlinear Supersonic Flutter of Circular Cylindrical Shells/
|
Amabili, M
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 71 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Novel Strategy for Suppressing the Flutter Oscillations of Aircraft Wings/
|
Hall, B D
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 72 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Optimized Nonuniform Rational B-Spline Geometrical Representation for Aerodynamic Design of Wings/
|
L�pine, J
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 73 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Response Surface Techniques for Diffuser Shape Optimization/
|
Madsen, J I
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 74 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Second-Order Classical Nonlinear Response Theory (TN)/
|
Ali, A H
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 75 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Separation Control by Alternating Tangential Blowing/Suction at Multiple Slots (TN)/
|
Sun, M
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 76 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Shear-Sensitive Liquid Crystal Coating Method Applied Through Transparent Test Surfaces (TN)/
|
Reda, D C
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 77 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Spanwise Variation in the Unsteady Stalling Flowfields of Two-Dimensional Airfoil Models/
|
Broeren, A P
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 78 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Spherical Particle Motion in Harmonic Stokes Flows/
|
Coimbra, C F M
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 79 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Stall Control with Local Surface Buzzing on a NACA 0012 Airfoil (TN)/
|
Park, Y W
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
| 80 |
|
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Swept Thin Wings in Unsteady Sonic Flow (TN)/
|
Soviero, P A O
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|
