Effects of fixing boundary-layer transition for a swept- and a triangular-wing and body combination at Mach numbers from 0.60 to 1.40
1960
28 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1959
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