Aircraft interior noise models: Sidewall trim, stiffened structures, and cabin acoustics with floor partition
As part of the continuing development of an aircraft interior noise prediction model, in which a discrete modal representation and power flow analysis are used, theoretical results are considered for inclusion of sidewall trim, stiffened structures, and cabin acoustics with floor partition. For vali...
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| Veröffentlicht in: | Journal of sound and vibration 1983-08, Vol.89 (3), p.371-417 |
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| container_end_page | 417 |
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| container_issue | 3 |
| container_start_page | 371 |
| container_title | Journal of sound and vibration |
| container_volume | 89 |
| creator | Pope, L.D. Wilby, E.G. Willis, C.M. Mayes, W.H. |
| description | As part of the continuing development of an aircraft interior noise prediction model, in which a discrete modal representation and power flow analysis are used, theoretical results are considered for inclusion of sidewall trim, stiffened structures, and cabin acoustics with floor partition. For validation purposes, predictions of the noise reductions for three test articles (a bare ring-stringer stiffened cylinder, an unstiffened cylinder with floor and insulation, and a ring-stringer stiffened cylinder with floor and sidewall trim) are compared with measurements. |
| doi_str_mv | 10.1016/0022-460X(83)90544-8 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0022-460X |
| ispartof | Journal of sound and vibration, 1983-08, Vol.89 (3), p.371-417 |
| issn | 0022-460X 1095-8568 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_23330480 |
| source | Access via ScienceDirect (Elsevier); NASA Technical Reports Server |
| subjects | Aircraft Design, Testing And Performance |
| title | Aircraft interior noise models: Sidewall trim, stiffened structures, and cabin acoustics with floor partition |
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