Nature of instability of helicopters is described, and factors that contribute to it are enumerated; two of A. M. YOUNG's early attempts to solve problem are discussed; final solution is device that makes model helicopters perfectly stable in flight; application of this device to full scale helicopters is also described. (Trans)
Helicopter stability with Young's lifting rotor
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 53 , n 12
1945
6 pages
Article (Journal)
English
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HELICOPTER STABILITY with Young's Lifting Rotor
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