| 21 |
|
Vibration Suppression Using Acceleration Feedback Control with Multiple Proof-Mass Actuators
|
Matunaga, S
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 22 |
|
Vibration Testing and Finite Element Analysis of an Inflatable Structure/
|
Park, G
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 23 |
|
Vibratory Characteristics of Pretwisted Cantilever Trapezoids of Unsymmetric Laminates
|
Liew, K. M
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 24 |
|
Viscoelastic Analysis of Thick-Walled Filament-Wound Composite Cylinderswith Elevated Temperatures
|
Tzeng, J. T
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 25 |
|
Viscoelastic Material Response with a Fractional-Derivative ConstitutiveModel
|
Baker, W. P
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 26 |
|
Viscous Drag Reduction Using Riblets on NACA 0012 Airfoil to Moderate Incidence
|
Sundaram, S
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 27 |
|
Viscous Flow Analysis Using a Parallel Unstructured Multigrid Solver/
|
Mavriplis, D J
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 28 |
|
Viscous Interaction Phenomena in Hypersonic Wedge Flow
|
De Luca, L
|
American Institute of Aeronautics and Astronautics
|
1995
|
|
|
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| 29 |
|
Viscous-Inviscid Interaction Using the Navier-Stokes Equations
|
Filippone, A
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 30 |
|
Visualization and Analysis of Bow Shocks in a Superorbital Expansion Tube
|
Wegener, M
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 31 |
|
Vortex Breakdown over Unsteady Delta Wings and Its Control
|
Yang, H
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 32 |
|
Vortex-Oscillation Model of Airfoil Side-Edge Noise
|
Sen, R
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
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| 33 |
|
Vortex Pairing as a Model for Jet Noise Generation
|
Leung, R. C. K
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 34 |
|
Vortex-Wake Characteristics of a Supersonic Transport Wing Plantform at Mach 2.5
|
Wang, F. Y
|
American Institute of Aeronautics and Astronautics
|
1996
|
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|
|