Open AccessHypersonic Shock Wave-Boundary-Layer Interaction on the Control Surface of a Slender Cone
Author(s) -
Anshuman Pandey,
Katya M. Casper,
Russell Spillers,
Melissa Marie Soehnel,
Seth Spitzer
Publication year - 2020
Publication title -
aiaa scitech 2022 forum
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2020-0815
Subject(s) - boundary layer , mach number , laminar flow , mechanics , flow separation , reynolds number , hypersonic speed , turbulence , physics , adverse pressure gradient , shock wave , oblique shock , freestream , optics , schlieren , materials science
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