タイトル | Validation of Vehicle Panel/Equipment Response from Diffuse Acoustic Field Excitation Using Spatially Correlated Transfer Function Approach |
本文(外部サイト) | http://hdl.handle.net/2060/20120014463 |
著者(英) | LaVerde, Bruce; Hunt, Ron; Fulcher, Clay; Smith, Andrew |
著者所属(英) | NASA Marshall Space Flight Center |
発行日 | 2012-04-23 |
言語 | eng |
内容記述 | An approach for predicting the vibration, strain, and force responses of a flight-like vehicle panel assembly to acoustic pressures is presented. Important validation for the approach is provided by comparison to ground test measurements in a reverberant chamber. The test article and the corresponding analytical model were assembled in several configurations to demonstrate the suitability of the approach for response predictions when the vehicle panel is integrated with equipment. Critical choices in the analysis necessary for convergence of the predicted and measured responses are illustrated through sensitivity studies. The methodology includes representation of spatial correlation of the pressure field over the panel surface. Therefore, it is possible to demonstrate the effects of hydrodynamic coincidence in the response. The sensitivity to pressure patch density clearly illustrates the onset of coincidence effects on the panel response predictions. |
NASA分類 | Acoustics |
レポートNO | M11-0877 |
権利 | Copyright, Distribution as joint owner in the copyright |