Analysis of unsteady inviscid diffuser flow with a shock wave

V. Yang, F. E.C. Culickt

研究成果: Article同行評審

25 引文 斯高帕斯(Scopus)

摘要

A finite difference scheme with a shock-fitting algorithm has been used to investigate unsteady inviscid flow with a shock in an inlet diffuser. The flowfield consists of three different regions: the supersonic and the subsonic regions, and a region containing both air and liquid fuel droplets, separated by a normal shock wave and a fuel injection system. The analysis is based on a two-phase, quasi-one-dimensional model. The response of a shock wave to various disturbances has been studied, including large-amplitude periodic oscillations and pulse perturbations.

原文English
頁(從 - 到)222-228
頁數7
期刊Journal of Propulsion and Power
1
發行號3
DOIs
出版狀態Published - 1985

All Science Journal Classification (ASJC) codes

  • 航空工程
  • 燃料技術
  • 機械工業
  • 空間與行星科學

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