Experimental and Numerical Study of Forced Shock-Wave Oscillations in a Transonic Channel.
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American Institute of Aeronautics and Astronautics |
7
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FUNDAMENTAL STUDY OF SHOCK WAVE/TURBULENT BOUNDARY LAYER INTERACTION WITH PASSIVE CONTROL IN TRANSONIC FLOW
National Aeronautics and Space Adminstration |
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EXPERIMENTAL INVESTIGATION OF THE RESPONSE OF A TRANSONIC SHOCK-WAVE TO DOWNSTREAM PERTURBATIONS
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
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A Numerical Study of an Oscillating Airfoil in Transonic Flows With Large Shock Wave Oscillations
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
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SHOCK WAVE/TURBULENT BOUNDARY LAYER INTERACTION IN THE FLOW FIELD OF A TRI-DIMENSION WIND TUNNEL
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |