Aerodynamic Analysis of a Spinning Missile with Dithering Canards Using a High Order Unstructured Grid Scheme
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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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Rolling Airframe Missile Aerodynamic Predictions Using a Chimera Approach for Dithering Canards.
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American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Efficient Implicit LU-SGS Algorithm for High-Order Spectral Difference Method on Unstructured Hexahedral Grids
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Aerodynamic Analysis of Complex Missile Configurations Using AVUS (Air Vehicles Unstructured Solver)
American Institute of Aeronautics and Astronautics |