Boundary-layer transition on a cooled 20° cone at Mach numbers of 1.5 and 2.0
1950
13 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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Boundary-layer transition on cooled 20° cone at mach numbers of 1.5 and 2.0
Engineering Index Backfile | 1950
|Boundary layer transition at hypersonic Mach numbers.
NTRS | 1967
|