Calculation of the three-dimensional flow field in supersonic inlets at angle of attack using a bicharacteristic method with discrete shock wave fitting
17th Aerospace Sciences Meeting ; 1979 ; New Orleans , LA , U.S.A.
01.01.1979
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Internal flow calculations for axisymmetric supersonic inlets at angle of attack
Tema Archiv | 1975
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