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Theoretical Analysis of an Annular Injection Supersonic Ejector Equipped with a Second-Throat

이차목을 갖는 환형 분사 초음속 이젝터 이론 해석

  • 김세훈 (한국과학기술원 항공우주공학과) ;
  • 진정근 (한국과학기술원 대학원 항공우주공학과) ;
  • 권세진 (한국과학기술원 항공우주공학과)
  • Published : 2005.12.01

Abstract

A theoretical analysis of an annular injection supersonic ejector equipped with a second-throat was developed under the assumption that the secondary flow is choked aerodynamically by interaction with primary flow in the mixing chamber. The predicted secondary flow pressure agrees reasonably well with the measurements. Using the analysis, the compression ratio, the secondary flow Mach number, and the location of the choking point were presented in terms of entrainment ratio.

Keywords

References

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