A NEW METHODOLOGY FOR PREDICTION OF SHOCK INTERSECTION LOCATION IN DOUBLE CONE SCRAMJET FOREBODIES (AIAA 2018-5317)
AIAA International Space Planes and Hypersonic Systems and Technolgies (Conference)
2018-01-01
8 pages
Aufsatz (Konferenz)
Englisch
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Hypersonic laminar-turbulent transition on circular cones and scramjet forebodies
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