NUMERICAL STUDY OF DETONATION PROPAGATION IN VISCOUS TURBULENT FLOW IN A DUCT

V. Sabelnikov, V. Vlasenko, S. Bakhne, S. S. Molev, A. Troshin, Onera French Aerospace Lab
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Abstract

Gasdynamics of detonation waves was widely studied within last hundred years - analytically, experimentally, and numerically. The majority of classical studies of the XX century were concentrated on inviscid aspects of detonation structure and propagation. There was a widespread opinion that detonation is such a fast phenomenon that viscous e¨ects should have insigni¦cant in§uence on its propagation. When the era of calculations based on the Reynolds-averaged Navier- Stokes (RANS) and large eddy simulation approaches came into effect, researchers pounced on practical problems with complex geometry and with the interaction of many physical effects. There is only a limited number of works studying the in§uence of viscosity on detonation propagation in supersonic §ows in ducts (i. e., in the presence of boundary layers).
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管道内粘性湍流爆轰传播的数值研究
在过去的一百年里,人们对爆震波的气体动力学进行了广泛的分析、实验和数值研究。20世纪的经典研究大多集中在爆轰结构和传播的非粘方面。人们普遍认为,爆炸是一种非常迅速的现象,黏性气流对爆炸传播的影响应该是微不足道的。当基于reynolds -average Navier- Stokes (RANS)和大涡模拟方法的计算时代开始生效时,研究人员开始研究复杂几何和许多物理效应相互作用的实际问题。研究粘度对超音速管道(即边界层存在下)爆轰传播的影响的工作数量有限。
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NUMERICAL STUDY OF DETONATION PROPAGATION IN VISCOUS TURBULENT FLOW IN A DUCT RANKING OF FUEL-AIR MIXTURES IN TERMS OF THEIR PROPENSITYTO DEFLAGRATION-TO-DETONATION TRANSITION THE SUPERSONIC ARGON FLOW PARAMETERS IN AN ARCJET THRUSTER PROPAGATION OF GASEOUS DETONATIONS IN PLANAR CURVED RECTANGULAR CHANNELS PULSE-DETONATION STEAM SUPERHEATER
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