| contributor author | J. F. Unruh | |
| contributor author | S. A. Dobosz | |
| date accessioned | 2017-05-08T23:28:52Z | |
| date available | 2017-05-08T23:28:52Z | |
| date copyright | April, 1988 | |
| date issued | 1988 | |
| identifier issn | 1048-9002 | |
| identifier other | JVACEK-28977#226_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/104788 | |
| description abstract | Detailed finite element models of a fuselage structure and acoustic cabin volume of a laboratory based prototypical aircraft fuselage were generated for the purpose of studying the predictive capabilities of deterministic modeling procedures for structure-borne noise transmission. Comparative predictions are made to measured wing-to-fuselage attach point inertances and interior noise to force responses. Several structural models with increased structural definition were evaluated. It was found that to accurately predict wing-to-fuselage attach point inertances required increased local area structural definition, while interior noise can be reasonably well predicted without paying additional attention to local area structural details. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Fuselage Structural-Acoustic Modeling for Structure-Borne Interior Noise Transmission | |
| type | Journal Paper | |
| journal volume | 110 | |
| journal issue | 2 | |
| journal title | Journal of Vibration and Acoustics | |
| identifier doi | 10.1115/1.3269503 | |
| journal fristpage | 226 | |
| journal lastpage | 233 | |
| identifier eissn | 1528-8927 | |
| keywords | Acoustics | |
| keywords | Noise (Sound) | |
| keywords | Modeling | |
| keywords | Wings | |
| keywords | Force | |
| keywords | Aircraft AND Finite element model | |
| tree | Journal of Vibration and Acoustics:;1988:;volume( 110 ):;issue: 002 | |
| contenttype | Fulltext | |
