Three-Dimensional Flow Separations on Aircraft and Missiles

This publication has 11 references indexed in Scilit:

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  AIAA Journal, 1968
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  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1968
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  AIAA Journal, 1968
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• Calculation of pressure distributions on cambered bodies of arbitrary cross section at angle of attack with application to transport fuselage afterbody design
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• The Determination of Turbulent Skin Friction by Means of Pitot Tubes
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