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Large-Eddy Simulation of air-fuel mixing in Dry Low NOx GTU Combustor

机译:干式低NOx GTU燃烧器中空燃混合的大涡模拟

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摘要

The in-house code FLAMENCO is developed to simulate the mixing process ina Dry Low NOx GTU Combustor. The physical approach is defined to model3D-unsteady, compressible, multi-species flows where turbulence plays a major role.For this purpose, Large Eddy-Simulation is applied in conjunction with high-orderschemes and stable formulation of volume fraction advection. Regarding the numericalstructure, FLAMENCO is a Finite-Volume Godunov-type algorithm equipped with5th and 2nd Order non-oscillatory reconstruction in space and 2nd Order, 4-StagesExplicit Runge-Kutta scheme for integration in time. From a mathematical pointof view, the multi-species approach is governed by the 5-Equation Transport Modeland is thermodynamically defined by iso-baric and perfect gas considerations, whichprevent pressure oscillations. Finally, an HLLC approximate Riemann solver computesconvective fluxes and 2nd Order centred differences accounts for dissipation terms.Previous research with an old version of FLAMENCO failed due to low dissipation in thejet injector tube. This issue stems from local energy being uncontrollably introduced inthis small region, leading to unphysical pressure values. It was found that the combinationof reflecting inflow, small cells and high gradients is responsible for acoustic wavereflection and amplification. To overcome this problem, a number of modificationsincluding boundary conditions (Partially Non-reflecting, Non-reflecting and Nozzle-typesubsonic inflows and outflows), an Adaptive Reconstruction Scheme, a more dissipativereconstruction scheme (5th Order WENO) and grid changes (only in jet injector) havebeen introduced. As a result, local energy generation and evacuation become balancedwithin physical boundaries, providing stable conditions in the whole domain.Initially, extensive validation of the new numerical approach is conducted throughcontrasted test cases such as Stationary and Moving Contact Wave, Shock Tube Problem,Kelvin-Helmholtz Instability and 2D-3D Explosion Problems. In the same way, strategiesintended to overcome the low dissipation problem are analysed in a representativeconfiguration. After the validation process, several simulations involving coarse andfine grids and different reconstruction schemes are run in the Dry Low NOx GTUCombustor. Finally, results are compared with experimental data, showing really goodaccuracy for 5th Order schemes, which is specially surprising in the coarse grid. Inthis way, highly turbulent, heterogeneous structures such as Vortex Breakdown, CentralRecirculation Zone, Precessing Vortex Core and Secondary Vortices are very wellcaptured, demonstrating the suitability of the mixing model to deal with highly turbulentflows where critical shear layers and high mixing ratios coexist in confined domains.
机译:内部代码FLAMENCO用于模拟干式低NOx GTU燃烧器的混合过程。物理方法定义为对湍流起主要作用的3D非稳态,可压缩,多物种流动建模,为此,将大涡模拟与高阶方案和体积分数对流的稳定公式结合应用。关于数值结构,FLAMENCO是有限体积的Godunov型算法,配备了空间的五阶和二阶非振荡重构以及二阶,四阶显式Runge-Kutta方案,可以及时进行积分。从数学观点来看,多物种方法受“ 5-方程输运模型”控制,并通过等压和理想气体考虑因素进行热力学定义,以防止压力波动。最后,一个HLLC近似Riemann求解器计算对流通量,并且二阶中心差解释了耗散项。以前的研究对旧版FLAMENCO的研究由于喷油嘴管中的低耗散而失败了。这个问题源于在这个小区域内不受控制地引入局部能量,从而导致了不自然的压力值。发现反射流,小细胞和高梯度的组合是声波反射和放大的原因。为了克服这个问题,进行了许多修改,包括边界条件(部分非反射,非反射和喷嘴型亚音速流入和流出),自适应重建方案,更具耗散性的重建方案(5阶WENO)和网格变化(仅在喷射中喷油器)已经引入结果,局部能量的产生和疏散在物理边界内变得平衡,从而在整个范围内提供了稳定的条件。最初,通过对比测试案例对新数值方法进行了广泛的验证,例如固定和移动接触波,激波管问题,开尔文-亥姆霍兹不稳定性和2D-3D爆炸问题。以相同的方式,在代表性配置中分析了旨在克服低耗散问题的策略。验证过程之后,在低NOx GTU燃烧室中进行了一些涉及粗略网格和精细网格以及不同重构方案的模拟。最后,将结果与实验数据进行比较,显示出5阶方案的准确性非常好,这在粗网格中尤其令人惊讶。这样,就很好地捕获了高度湍流的非均质结构,例如涡旋破坏区,中央再循环区,旋进涡旋核心和次要涡旋,这表明混合模型适用于处理高湍流,其中临界剪切层和高混合比共存于密闭区域。

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    Aguado Pablo;

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  • 年度 2014
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  • 正文语种 {"code":"en","name":"English","id":9}
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