Response of a helicopter rotor to oscillatory pitch and throttle movements
1949
31 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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English
Response of helicopter rotor to oscillatory pitch and throttle movements
Engineering Index Backfile | 1949
|Helicopter rotor wing variable-pitch rod, helicopter automatic inclinator and helicopter
European Patent Office | 2020
|