Aircraft Structure’s Response Prediction Analysis and Experimental Study in High-strength Broadband Noise Environments

Since dynamic environment of the hypersonic aircraft has a wide frequency domain, it is difficult to predict the vibration response with finite element methods. A certain type of high-speed aircraft's vibro-acoustic dynamics model is established based on statistical energy analysis (SEA) theory...

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Bibliographische Detailangaben

Veröffentlicht in:	Ji xie gong cheng xue bao 2016-01, Vol.52 (3), p.71-78
1. Verfasser:	LIN, Huagang
Format:	Artikel
Sprache:	chi ; eng
Schlagworte:	Aircraft Design engineering Dynamic models Mathematical analysis Mathematical models Noise Noise prediction (aircraft) Optimization
Online-Zugang:	Volltext
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