A preliminary analytical method for predicting whether rotor blade bang will occur is described and correlated with data from tandem rotor helicopters. The operating limits which will cause banging of a single rotor are discussed. (Author)
Helicopter Rotor Noise Analysis
1966
65 pages
Report
Keine Angabe
Englisch
Helicopter rotor thickness noise
AIAA | 1980
|AIAA | 1986
|Helicopter rotor noise generation.
NTRS | 1969
|Helicopter Rotor Thickness Noise
AIAA | 1981
|Helicopter rotor thickness noise
Tema Archiv | 1980
|