Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94
1957
29 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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Engineering Index Backfile | 1961
|Engineering Index Backfile | 1960
|