Noise test and simulation of military aircraft

Wen Zhong Lou*, Jie Qiao

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

2 引用 (Scopus)

摘要

Based on the demand for noise control and protection, a study on the noise diffuse and intensity of military aircraft is carried out. A boundary element model is established, making use of the ANSYS. In the noise simulation SYSNOISE is applied to get estimable simulation results of aircraft noise close to ground. A minitype wireless noise measure system is designed to act as an automonitor, which has been proved to be a practical device.

源语言英语
页(从-至)295-298+317
期刊Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
27
4
出版状态已出版 - 4月 2007

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