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
Article (Journal)
English
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The stability of rotor blade flapping motion
TIBKAT | 1961
|The stability of rotor blade flapping motion
SLUB | 1961
|Rotor Blade Flapping Criteria Investigation
NTIS | 1976
|Helicopter Rotor Blade Flapping and Bending
Emerald Group Publishing | 1957
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