Distributive loading rotational theory for helicopter rotor noise generation, considering steady and fluctuating force radiation and impulsive blade slap
Helicopter rotor noise generation.
AERODYNAMICS OF ROTARY WING AND V/STOL AIRCRAFT, SYMPOSIUM ; 1969 ; BUFFALO, NY
1969-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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