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[American Institute of Aeronautics and Astronautics 17th Aerospace Sciences Meeting - New Orleans,LA,U.S.A. (15 January 1979 - 17 January 1979)] 17th Aerospace Sciences Meeting - Calculation of the three-dimensional flow field in supersonic inlets at angle of attack using a bicharacteristic method with discrete shock wave fitting

โœ Scribed by VADYAK, J.; HOFFMAN, J.; BISHOP, A.


Book ID
121027393
Publisher
American Institute of Aeronautics and Astronautics
Year
1979
Weight
714 KB
Category
Article

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