Direct Numerical Simulations of laminar-turbulent boundary-layer transition for blunt cones at Mach 6: Effect of Varying Nose Bluntness
AIAA AVIATION 2021 FORUM
01.01.2021
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
EFFECT OF NOSE BLUNTNESS ON HYPERSONIC BOUNDARY LAYER RECEPTIVITY OVER A BLUNT CONE
British Library Conference Proceedings | 2005
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