Effect of a Normal Shock Wave on Freestream Total Pressure Fluctuations in a Low-Density Mach 6 Flow
44th AIAA Fluid Dynamics Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of a Normal Shock Wave on Freestream Total Pressure Fluctuations in a Low-Density Mach 6 Flow
British Library Conference Proceedings | 2014
|Review of wind-tunnel freestream pressure fluctuations
AIAA | 1977
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