Transitional Shock Wave-Boundary Layer Interaction over a Cone Flare Model at Hypersonic Conditions

Details Transitional Shock Wave-Boundary Layer Interaction over a Cone Flare Model at Hypersonic Conditions Transitional Shock Wave-Boundary Layer Interaction over a Cone Flare Model at Hypersonic Conditions

Feb 2002

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002esasp.487..725a&link_type=gif

Fourth Symposium on Aerothermodynamics for Space Vehicles: co-sponsored by European Space Agency. Held October 15-18, 2001, in C

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