Theoretical analysis of an airplane acceleration restrictor controlled by normal acceleration, pitching acceleration, and pitching velocity
1954
42 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1954
|Numerical Representation of Pitching and Non-Pitching Airfoils Undergoing Linear Acceleration
British Library Conference Proceedings | 1997
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