• 제목/요약/키워드: Rankine-Hugoniot relation

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경사 데토네이션파의 근사 해석 모델과 비정상 상세구조 (Approximate Analysis Model and Detailed Unsteady Structure of Oblique Detonation Waves)

  • 최정열;김동완
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제25회 추계학술대회논문집
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    • pp.136-140
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    • 2005
  • 일차원 ZND 데토네이션 구조 해석 모델의 연장선상에서 경사 충격파와 경사 데토네이션 파에 대하여 Rankine-Hugoniot 관계식과 반응속도를 연계한 이차원 경사 데토네이션 파의 구조해석 모델을 제시하였다. 이에 기반을 두어 삼중점, 횡단 충격파 및 셀 구조를 포함하는 경사 데토네이션 파의 비정상 상세 구조를 조사하기 위한 이차원 유체역학 해석을 수행하였다. 전산 유체 해석 결과는 경사 데토네이션 파의 상세구조에 대한 깊이 있는 이해를 제공하며, 해석 모델은 경사 데토네이션 파를 연소 메커니즘으로 이용하는 극초음속 추진기관의 통합 설계도구로 이용될 수 있을 것이다.

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쐐기 및 원추 주위의 불안정한 충격파 유도연소 해석 (Analysis of Unstable Shock-Induced Combustion over Wedges and Conical Bodies)

  • Jeong-Yeol Choi
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.32-33
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    • 2003
  • Mechanism of a periodic oscillation of shock-induced combustion over a two- dimensional wedges and axi-symmetric cones were investigated through a series of numerical simulations at off-attaching condition of oblique detonation waves(ODW). A same computational domain over 40 degree half-angle was considered for two-dimensional and axi-symmetric shock-induced combustion phenomena. For two-dimensional shock-induced combustion, a 2H2+02+17N2 mixture was considered at Mach number was 5.85with initial temperature 292 K and initial pressureof 12 KPa. The Rankine-Hugoniot relation has solution of attached waves at this condition. For axi-symmetric shock-induced combustion, a H2+2O2+2Ar mixture was considered at Mach number was 5.0 with initial temperature 288 K and initial pressure of 200 mmHg. The flow conditions were based on the conditions of similar experiments and numerical studies.[1, 3]Numerical simulation was carried out with a compressible fluid dynamics code with a detailed hydrogen-oxygen combustion mechanism.[4, 5] A series of calculations were carried out by changing the fluid dynamic time scale. The length wedge is varied as a simplest way of changing the fluid dynamic time scale. Result reveals that there is a chemical kinetic limit of the detached overdriven detonation wave, in addition to the theoretical limit predicted by Rankine-Hugoniot theory with equilibrium chemistry. At the off-attaching condition of ODW the shock and reaction waves still attach at a wedge as a periodically oscillating oblique shock-induced combustion, if the Rankine-Hugoniot limit of detachment isbut the chemical kinetic limit is not.Mechanism of the periodic oscillation is considered as interactions between shock and reaction waves coupled with chemical kinetic effects. There were various regimes of the periodicmotion depending on the fluid dynamic time scales. The difference between the two-dimensional and axi-symmetric simulations were distinct because the flow path is parallel and uniform behind the oblique shock waves, but is not behind the conical shock waves. The shock-induced combustion behind the conical shockwaves showed much more violent and irregular characteristics.From the investigation of characteristic chemical time, condition of the periodic instability is identified as follows; at the detaching condition of Rankine-Hugoniot theory, (1) flow residence time is smaller than the chemical characteristic time, behind the detached shock wave with heat addition, (2) flow residence time should be greater than the chemical characteristic time, behind an oblique shock wave without heat addition.

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DELTA-SHOCK FOR THE NONHOMOGENEOUS PRESSURELESS EULER SYSTEM

  • Shiwei Li;Jianli Zhao
    • 대한수학회보
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    • 제61권3호
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    • pp.699-715
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    • 2024
  • We study the Riemann problem for the pressureless Euler system with the source term depending on the time. By means of the variable substitution, two kinds of Riemann solutions including deltashock and vacuum are constructed. The generalized Rankine-Hugoniot relation and entropy condition of the delta-shock are clarified. Because of the source term, the Riemann solutions are non-self-similar. Moreover, we propose a time-dependent viscous system to show all of the existence, uniqueness and stability of solutions involving the delta-shock by the vanishing viscosity method.