The supersonic pressure drag of a swept wing with a cranked maximum thickness line
1951
29 S., 1 Tab., 7 S. Abb.
4"
[Umschlagt.]
[Text mschr. autogr.]
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Tests of fairing to reduce drag of supersonic swept-wing root
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