Pressure distribution and damping in steady pitch at supersonic Mach numbers of flat swept-back wings having all edges subsonic
1950
62 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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English
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1950
|