Tests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, andthe Clark Y sections
1933
8 S., [5] Bl
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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English
Tests of three tapered airfoils based on N.A.C.A. 2200 N.A.C.A.-M6, and Clark Y sections
Engineering Index Backfile | 1934
|Tests of N.A.C.A. Airfoils in variable-density wind tunnel
Engineering Index Backfile | 1936
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