Laminar boundary-layer separation induced by flares on cylinders with highly cooled boundary layers at a Mach number of 15
1965
31 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Stability of highly-cooled compressible laminar boundary layers
Tema Archive | 1976
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