Supersonic Laminar Flow Control on Swept Wings Using Distributed Roughness.
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American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
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 |
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In-Flight Receptivity Experiments on a 30-Degree Swept-Wing using Micron-Sized Discrete Roughness Elements
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |