A laboratory test apparatus was developed which would allow the study and development of propeller wake/vortex-induced structure-borne interior noise control measures. Various methods of wing structural modification, including blocking masses, surface damping treatments, and tuned mechanical absorbers, were evaluated relative to reduced interior noise levels. Inboard wing fuel was found to act as an effective blocking mass. Wing panel add-on damping treatment in the form of a single, constrained layer was not an effective control measure, except in the area of the propeller wake. However, highly damped, tuned mechanical absorbers were found to be the most efficient structure-borne noise (SBN) control measure.
Structure-borne noise control for propeller aircraft
1987-10-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Structure-borne noise control for propeller aircraft
AIAA | 1988
|Structure-borne noise control for propeller aircraft
NTRS | 1988
|Structure-borne noise control for propeller aircraft
AIAA | 1987
|Aircraft propeller induced structure-borne noise
NTRS | 1989
|Aircraft Propeller Induced Structure-Borne Noise
NTIS | 1989
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