This paper presents results of a systematic experimental investigation of parameters which affect sound transmission through general aviation structures. Parameters studied include angle of sound incidence, panel curvature, panel stresses, and edge conditions for bare panels; pane thickness, spacing, inclination of window panes, and depressurization for dual pane windows; densities of hard foam and sound absorption materials, air gaps, and trim panel thickness for multilayered panels. Based on the study, some promising methods for reducing interior noise in general aviation airplanes are discussed.
Summary of Typical Parameters that Affect Sound Transmission through General Aviation Aircraft Structures
Sae Technical Papers
Business Aircraft Meeting and Exposition ; 1981
1981-02-01
Aufsatz (Konferenz)
Englisch
Typical General Aviation Aircraft
NTIS | 1999
|The Typical General Aviation Aircraft
NTRS | 1999
|