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Towards predicting supersonic, hot jet noise

  • Thaerocomp Technical Corporation
  • AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The noise from supersonic jet aircraft during landing and taking-off poses serious environmental challenge to military bases. Two RANS-based acoustic source models have been used to calculate the noise signature from a supersonic, hot jet flow, one is based on the MGBK method from Khavaran et al. [12] and the other one is from Tarn and Auriault[13]. The aerodynamic predictions from our RANS calculation with high-order numerical schemes and modified k-s models agree well with experimental data. However, it is found that both acoustic models have only limited success in predicting the far-field sound spectrum especially for shallow aft-angles, while the MGBK method has a slightly better performance over Tam's method for the prediction of overall sound pressure levels. The large-eddy simulation approach is suggested to use for predicting supersonic, hot jet noise.

Original languageEnglish
Title of host publicationCollection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
Pages10028-10043
Number of pages16
StatePublished - 2007
Event45th AIAA Aerospace Sciences Meeting 2007 - Reno, NV, United States
Duration: Jan 8 2007Jan 11 2007

Publication series

NameCollection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
Volume15

Conference

Conference45th AIAA Aerospace Sciences Meeting 2007
Country/TerritoryUnited States
CityReno, NV
Period01/8/0701/11/07

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