Dynamic modeling and numerical simulation of acoustic-thermal-fluid coupling for hypersonic vehicle fatigue test: 19th AIAA/CEAS Aeroacoustics Conference

W. Yu, S. Zhong, X. Huang

Research output: Unpublished conference presentation (presented paper, abstract, poster)Conference presentation (not published in journal/proceeding/book)Academic researchpeer-review

Abstract

A control-oriented dynamic model for acoustic-thermal- fluid coupling problem in thermal- acoustic fatigue testing facility was presented in this paper. By this control-oriented model, transient dynamic process of multi-physics coupling problem in a progressive wave tube could be approximately studied. The proposed model is verified by comparing to computational results using acoustic and fluid computational tools. We found that the proposed modeling method is much faster than classical acoustic and fluid computational methods. The modeling result agrees largely well with the computational results. The potential reasons of the modeling errors are discussed in this paper. Then, the model should be useful in fatigue testing preparation and evaluations.
Original languageEnglish
DOIs
Publication statusPublished - 2013

Keywords

  • Aeroacoustics
  • Computational methods
  • Fatigue testing
  • Computational results
  • Computational tools
  • Control oriented models
  • Multi-physics couplings
  • Progressive wave tubes
  • Testing facility
  • Thermal acoustics
  • Transient dynamics
  • Hypersonic vehicles

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