A response analysis is carried out to determine the predictability of sidewall accelerations in aircraft, to investigate whether it is necessary to model the exterior pressure as a traveling wave as opposed to a standing wave, and to determine the importance of parameters describing the exterior pressure and sidewall panel. Prediction of the acceleration response is found to be improved by including traveling wave and spatial variation effects of the exterior pressure in the model. Variations with propeller rpm are found to be important for the longer panel.
Acceleration response of fuselage sidewall panels on a twin-engine, light aircraft
In: Noise-Con 81 ; 1981 ; Raleigh, NC
1981-01-01
Miscellaneous
No indication
English
NTRS | 1982
|AIRCRAFT FUSELAGE ASSEMBLY JIG AND METHOD FOR HANDLING AIRCRAFT FUSELAGE PANELS
European Patent Office | 2017
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