Experimental and Numerical Investigation of Unsteady Shock Wave Interaction with a Thruster Cavity in Mach 7 Flow Over 30° Wedge
AIAA SCITECH 2022 Forum
2022-01-01
Conference paper
Electronic Resource
English
Shock Wave Laminar Boundary Layer Interaction Over a Double Wedge in a High Mach Number Flow
British Library Conference Proceedings | 2014
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