Boundary-layer receptivity and breakdown in hypersonic flow over a swept blunt wedge with three-dimensional freestream acoustic disturbances
8th AIAA Flow Control Conference
01.01.2016
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Receptivity of Boundary Layer over a Blunt Wedge due to Freestream Pulse Disturbances at Mach 6
DOAJ | 2016
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