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Concurrent Experimental and Computational Study of Combustion Dynamics in a Single-Element Lean Direct Injection (LDI) Gas Turbine Combustor

机译:单元素贫液(LDI)燃气轮机燃烧器中燃烧动力学的并发实验和计算研究

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A concurrent effort comprising simulation and experiment to assess the ability of high-fidelity models to predict combustion dynamics in a high pressure (1 MPa) liquid fueled lean direct inject (LDI) combustor are presented in the paper. Results from experiment and computations at an inlet air temperature of 800 K and an equivalence ratio of 0.6 are described. High frequency wall pressure and 10 kHz OH-PLIF measurements from experiment are compared with corresponding wall pressure, heat release and OH mass fraction results from hybrid RANS-LES simulations using both 2-step global and a reduced 18-reaction kinetics model. A dominant mode in the 1450-1650 Hz range- corresponding to the 4L chamber mode- is observed in the combustor, both in experiments and simulations, with a pressure fluctuation amplitude of ~10% P'/Pc. Dynamic Mode Decomposition (DMD) of the OH-PLIF data and the simulation results identify similar dominant unstable modes in the combustor.
机译:一种并发努力,包括仿真和实验,以评估高保真模型在纸上提出了高压(1MPa)燃料稀释直接注射(LDI)燃烧器中的燃烧动力学的能力。描述了从800 k的入口空气温度的实验和计算结果和0.6的等效比。使用两步全局和减少的18-反应动力学模型将来自实验的高频壁压和10kHz OH-PLIF测量与实验中的10kHz OH-PLIF测量与杂交rans-les仿真相比。在实验和模拟中,在燃烧器中观察到1450-1650 Hz中的主导模式 - 在燃烧器中观察到燃烧器中,压力波动幅度为约10%P'/ PC。 OH-PLIF数据的动态模式分解(DMD)和仿真结果识别燃烧器中的类似显性不稳定模式。

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