A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls
Wartime report ; L-302
1942
13 S., [3] Bl
graph. Darst
Originally issued February 1942 as Advance restricted report
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
Englisch
Engineering Index Backfile | 1942
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