Rapid Method for Computing Reachable Landing Distances in Helicopter Autorotative Descent
Journal of Aerospace Information Systems ; 19 , 7 ; 504-510
01.07.2022
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Analysis of transition of helicopter from hovering to steady autorotative vertical descent
Engineering Index Backfile | 1949
|Electrically powered rotorcraft capable of autorotative landing
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