Method for solution of class of Hill differential equations is applied to solution of equation for flapping motion of helicopter rotor blades; stability of blade flapping motion is established for range of numerical parameters usually arising in helicopter theory.
Rotor blade flapping motion
Brown Univ -- Quarterly Applied Mathematics
Quarterly of Applied Mathematics ; 5 , n 2
1947
19 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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