21 |
|
FLOW CONTROL - Compressible Dynamic Stall Control: Comparison of Two Approaches/
|
Chandrasekhara, M S
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
22 |
|
FLOW CONTROL - Computational Analysis of Centrifugal Compressor Surge Control Using Air Injection/
|
Stein, A
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
23 |
|
FLOW CONTROL - Dynamic Stall Control by Periodic Excitation, Part 1: NACA 0015 Parametric Study/
|
Greenblatt, D
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
24 |
|
FLOW CONTROL - Dynamic Stall Control by Periodic Excitation, Part 2: Mechanisms/
|
Greenblatt, D
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
25 |
|
FLOW CONTROL - Flow Control: The Future/
|
Gad-el-Hak, M
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
26 |
|
FLOW CONTROL - Flow Separation Control with Microflexural Wall Vibrations/
|
Sinha, S K
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
27 |
|
FLOW CONTROL - Micro-Air-Vehicles: Can They be Controlled Better?/
|
Gad-el-Hak, M
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
28 |
|
FLOW CONTROL - Microblowing for High-Angle-of-Attack Vortex Flow Control on a Fighter Aircraft/
|
Roos, F W
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
29 |
|
FLOW CONTROL - Numerical Simulation of Enhanced Mixing in Jet Plumes Using Pulsed Blowing/
|
Smith, T D
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
30 |
|
FLOW CONTROL - Oscillatory Control of Shock-Induced Separation/
|
Seifert, A
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
31 |
|
Flow Control over a Maneuvering Delta Wing at High Angles of Attack
|
Klute, S. M
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
32 |
|
FLOW CONTROL - Periodic Excitation for Jet Vectoring and Enhanced Spreading/
|
Pack, L G
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
33 |
|
FLOW CONTROL - Physical Analysis and Scaling of a Jet and Vortex Actuator (EN)/
|
Lachowicz, J T
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
34 |
|
FLOW CONTROL - Progress on the Use of Compliant Walls for Laminar-Flow Control/
|
Carpenter, P W
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
35 |
|
Flowfield Measurements Inside a Boundary-Layer Bleed Slot
|
Davis, D. O
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
36 |
|
Flowfield Surveys and Computations of a Crossing-Shock Wave/Boundary-Layer Interaction
|
Garrison, T. J
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
37 |
|
Flow Model for Predicting Normal Shock Wave Induced Vortex Breakdown
|
Smart, M. K
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
38 |
|
Flow Oscillation over an Airfoil Near Stall (TN)
|
Bragg, M. P
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
39 |
|
Flow over an Obstacle Emerging from the Wall of a Channel
|
Carlson, H. A
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
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40 |
|
Flow Visualization of an Oscillating Airfoil with Sawtooth Trailing Edge
|
Myose, R. Y
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
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