Pressure-gradient effects on hypersonic turbulent skin friction and boundary-layer profiles
10th Aerospace Sciences Meeting ; 1972 ; San Diego , CA , U.S.A.
01.01.1972
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion
British Library Conference Proceedings | 2005
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