Elementary calculation inspired by classic treatment for steady state permits determination of induced velocity and overall lift of rotor as function of collective pitch for all values of advance per turn; nature of lift response is shown to be function of rate of pitch change. Translated from Acad des Sciences -- Comptes Rendus, Sept 1 1958.
Response of rotor lift to increase in collective pitch in case of descending flight, regime of rotor being near autorotation
NASA -- Tech Translation
1960
5 pages
Report
English
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