Method for rapid calculation of higher harmonics of rotor blade flapping and bending; solution of large numbers of simultaneous equations is eliminated and it is possible to complete most of calculation without introducing actual value of tip speed ratio. (See also - n 337 Mar 1957 p 64-66)
Helicopter rotor blade flapping and bending
Aircraft Eng
Aircraft Engineering ; 29 , n 338
1957
6 pages
Aufsatz (Zeitschrift)
Englisch
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