Noise test and simulation of military aircraft

Wen Zhong Lou*, Jie Qiao

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

2 Citations (Scopus)

Abstract

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.

Original languageEnglish
Pages (from-to)295-298+317
JournalBeijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
Volume27
Issue number4
Publication statusPublished - Apr 2007

Keywords

  • Aircraft noise
  • Noise simulation
  • Wireless communication

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