Nondimensional Analysis of Periodically Unstable Shock-Induced Combustion

주기적 불안정성을 가지는 충격파 유도 연소의 무차원 해석

  • 최정열 (서울대학교 항공우주공학과) ;
  • 정인석 (서울대학교 항공우주공학과) ;
  • 윤영빈 (서울대학교 항공우주공학과)
  • Published : 1996.12.31

Abstract

A numerical study is conducted to investigate the periodically unstable shock induced combustion around blunt bodies in stoichiometric hydrogen-air mixtures. Euler equations are spatially discretized by upwind-biased third order scheme and temporally integrated by Runge-Kutta method. Chemistry model used in this study involves 8 elementary kinetics steps and 7 species. At a constant Mach number, the effects of projectile size, inflow pressure and inflow temperature are examined with Lehr#s experimental condition as a reference. In addition to oscillation frequency, characteristic distances and time averaged values are found from the result to find an relation with dimensionless parameters. As a result, it is found that the effects of inflow pressure and body size are very similar and $Damk{\ddot{o}}hler$ number plays an important role in determining the instability characteristics.

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