Flight measurements of aerodynamic noise were made on an AeroCommander airplane with engines off and a JetStar airplane with engines at both idle power and completely shut off. The overall sound level for these airplanes in the landing configuration varied as the sixth power of the aircraft velocity. For the JetStar airplane, the overall sound level decreased as the inverse square of the distance in the lateral direction. The aerodynamic noise was approximately 11 decibels below the FAR Part 36 noise level for the JetStar airplane. The landing gear were a significant contributor to aerodynamic noise for both aircraft.
Preliminary measurements of aircraft aerodynamic noise
Fluid and Plasma Dynamics Conference ; 1974 ; Palo Alto, CA
1974-06-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Preliminary measurements of aircraft aerodynamic noise
AIAA | 1974
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