For low speed rotors, it is shown that unsteady load models are only partially successful in predicting experimental levels. A theoretical model is presented which leads to the concept of unsteady thickness noise. This gives better agreement with test results. For high speed rotors, it is argued that present models are incomplete and that other mechanisms are at work. Some possibilities are briefly discussed.
Theoretical models of helicopter rotor noise
01.08.1978
Aufsatz (Konferenz)
Keine Angabe
Englisch
Helicopter rotor thickness noise
AIAA | 1980
|Helicopter Rotor Thickness Noise
AIAA | 1981
|Helicopter rotor thickness noise
Tema Archiv | 1980
|AIAA | 1986
|Helicopter rotor noise generation.
NTRS | 1969
|