Shock / Boundary-Layer Interaction Control Using Three-Dimensional Bumps in Supersonic Engine Inlets
46th AIAA Aerospace Sciences Meeting and Exhibit
2008-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Shock-Wave-Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings
Online Contents | 2008
|British Library Conference Proceedings | 2007
|Three dimensional optimization of supersonic inlets
AIAA | 1999
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