The dynamic-response characteristics of a 35 [degree] swept-wing airplane as determined from flight measurements
1955
25 S
graph. Darst
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Buch
Englisch
Dynamic-response characteristics of 35° swept-wing airplane as determined from flight measurements
Engineering Index Backfile | 1955
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