Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
1956
75 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1956
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British Library Conference Proceedings | 2009
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