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LES model of large scale hydrogen-air planar detonations: Verification by the ZND theory

机译:大规模氢-空气平面爆轰的LES模型:ZND理论验证

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The large eddy simulation (LES) model of hydrogen-air detonation at very large scales, which doesn't require Arrhenius chemistry, is presented. The progress variable equation is applied for the first time to simulate propagation of a reaction front following and coupled with a leading shock. The gradient method, based on a product of pre-shock mixture density and detonation velocity, is employed as a source term in the progress variable equation. Chemical kinetics enters the combustion model only through its influence on the detonation velocity and modelling of detailed chemistry is omitted. The LES model is verified against theoretical solution by the Zel'dovich-von Neumann-Doring (ZND) theory for a case of planar 29.05% hydrogen-air detonation in elongated 3 × 3 × 100 m calculation domain. Thermodynamically calculated values of the specific heats ratio for burned mixture γ = 1.22 and the standard heat of combustion △H_c = 3.2 MJ/kg are applied without any adjustment often applied in other models. Numerical simulation reproduced theoretical values of von Neumann spike, Chapman-Jouguet pressure, Taylor wave and detonation propagation velocity. There are no adjustable parameters in the model. Practically no grid sensitivity for the planar detonation wave is demonstrated by the LES model. Detonation velocity and pressures are shown to be nearly independent of the computational cell size in a wide range of cell sizes 0.1-1.0 m. Impulse depends to some extent on a cell size. Three-dimensional version of the LES model is under development to simulate pressure effects and identify design solutions, including mitigating techniques, for hydrogen safety engineering. There is no intention to use this oriented on large scale applications engineering LES model to reproduce fine structure of the detonation wave.
机译:提出了不需要Arrhenius化学的大规模氢-空气爆轰的大涡模拟(LES)模型。首次应用进度变量方程来模拟跟随并与前导冲击耦合的反应前沿的传播。基于预震混合物密度和爆速的乘积的梯度法被用作进度变量方程中的源项。化学动力学仅通过其对爆炸速度的影响而进入燃烧模型,因此省略了详细化学模型的建模。 LES模型通过Zel'dovich-von Neumann-Doring(ZND)理论针对理论解进行验证,适用于在3×3×100 m加长计算域中平面29.05%氢-空气爆轰的情况。使用燃烧混合物的比热比γ= 1.22和标准燃烧热△H_c = 3.2 MJ / kg的热力学计算值,而无需在其他模型中经常进行任何调整。数值模拟再现了冯·诺伊曼峰,查普曼-乔格压力,泰勒波和爆轰传播速度的理论值。模型中没有可调参数。 LES模型几乎没有证明平面爆轰波的网格灵敏度。爆炸速度和爆破压力在0.1-1.0 m的大范围内几乎与计算单元大小无关。冲动在某种程度上取决于细胞的大小。 LES模型的三维版本正在开发中,以模拟压力影响并确定用于氢安全工程的设计解决方案,包括缓解技术。无意使用面向大规模应用工程的LES模型来重现爆炸波的精细结构。

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