Experimental laminar, transitional, and turbulent boundary-layer profiles on a wedge at local mach number 6.5 and comparisons with theory
1971
58 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Shock Wave Laminar Boundary Layer Interaction Over a Double Wedge in a High Mach Number Flow
British Library Conference Proceedings | 2014
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