Analogue/Digital Wind Tunnel Testing of Active Low Momentum Flow Control on Single and Multi-Component Airfoil Systems at High Lift.
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
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テクニカルペーパー
Active Aeroelastic Control over a Multi-Surface Wing: Modelling and Wind Tunnel Testing
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |