Response of a helicopter rotor to an increase in collective pitch for the case of vertical flight
Réponse d'un rotor d'hélicoptère a une augmentation du pas général dans le cas du vol vertical <engl.>
1961
20 S., [2] Bl
Ill., graph. Darst
Übers. aus: Technique et science aéronautiques ; 1959,3
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Response of helicopter rotor to increase in collective pitch for case of vertical flight
Engineering Index Backfile | 1961
|ASSISTED COLLECTIVE PITCH CONTROL SYSTEM FOR A HELICOPTER ROTOR
European Patent Office | 2023
|Engineering Index Backfile | 1960
|Engineering Index Backfile | 1960
|