基于平行自适应网格细化的旋转爆震波高分辨率数值模拟

IF 5 Q2 ENERGY & FUELS
Han Peng , Ralf Deiterding
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引用次数: 0

摘要

旋转爆震发动机的模拟仍然主要是在均匀网格或静态精细网格上求解。本文采用块结构自适应网格细化(SAMR)技术对预混旋转爆震波进行了模拟。所研究的构型包括二维离散注入氢-空气混合气展开模型和三维未预混和部分预混氢-空气混合气环形模型。计算采用了平行笛卡尔自适应网格细化框架AMROC中的通用求解器,该框架已扩展到适应曲线网格。采用二阶精确有限体积法求解Navier-Stokes方程,并采用网格对齐的Riemann求解热完美气体混合物。详细的,多步骤的化学动力学机制被采用,并结合了分裂的方法。对网格依赖性进行了研究,评估了局部网格细化和自适应准则对仿真结果的影响。分析揭示了多波结构和瞬态热释放模式的形成,表明当爆轰通过喷射射流传播时,存在不规则的细胞结构和增强的局部热释放。能够将亚尺度现象分解到细胞结构,这是爆轰传播固有的,证明了SAMR方法的好处。进一步模拟研究了部分预混对旋转爆轰的影响。此外,工作负载分布分析演示了AMROC中的动态分区策略如何减轻计算不平衡。平行缩放测试在解决旋转爆震发动机问题时表现出线性加速,突出了平行自适应网格细化技术在捕获这些模拟的主要特征方面的效率。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
High-resolution numerical simulation of rotating detonation waves with parallel adaptive mesh refinement
Simulations of rotating detonation engines are still dominated by solvers on uniform or statically refined meshes. Here, simulations of premixed rotating detonation waves are conducted using the block-structured adaptive mesh refinement (SAMR) technique. The studied configurations include both a two-dimensional unrolled model with a discretely injected hydrogen-air mixture and a three-dimensional annular model with non-premixed and partially premixed hydrogen-air mixtures. The computations employ a generic solver within the parallel Cartesian adaptive mesh refinement framework AMROC, which has been extended to accommodate curvilinear meshes. A second-order accurate finite volume method for the Navier–Stokes equations is utilized, along with grid-aligned Riemann solvers for thermally perfect gas mixtures. Detailed, multi-step chemical kinetic mechanisms are employed and incorporated with a splitting approach. A study into mesh dependency is undertaken, providing an assessment of the influence of local mesh refinement and adaptation criteria on the simulation results. The analysis reveals the formation of a multi-wave structure and transient heat release patterns, indicating the presence of an irregular cellular structure with enhanced local heat release as the detonation propagates through the injection jets. The ability to resolve sub-scale phenomena down to the cellular structures, intrinsic to detonation propagation, demonstrates the benefit of the SAMR approach. Further simulations are conducted to investigate the effects of partial premixing on rotating detonation. Additionally, a workload distribution analysis demonstrates how the on-the-fly partition strategy in AMROC alleviates computational imbalances. Parallel scaling tests exhibit linear acceleration in solving rotating detonation engine problems, highlighting the efficiency of the parallel adaptive mesh refinement technique in capturing the primary features of these simulations.
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4.20
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