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Coupling Heat Transfer and Fluid Flow Solvers for Multidisciplinary Simulations

机译:耦合传热和流体流动求解器,用于多学科模拟

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摘要

The feasibility of multidisciplinary simulations for realistic geometries involving detailed physical models is demonstrated. Specifically, a three-dimensional chemically reacting fluid flow solver is coupled with a solid-phase heat transfer solver that includes cooling channels. Both fluid- and solid-phase models employ the integral, conservative form of the governing equations and are discretized by means of two finite volume numerical schemes. To keep the heat flux consistent, a special algorithm is developed at the interface between the solid and fluid regions. Physical and thermal properties of the solid materials can be temperature dependent, and different materials can be used in different parts of the domains due to a multiblock gridding strategy. The cooling channel model is developed by using conservation laws of mass, momentum, and energy, taking into account the effects of heat transfer and friction. The coupling of the models (solid and fluid, solid and cooling channels) is detailed. A hot-air nozzle test case is examined, and the simulated results are validated by means of available experimental data. Finally, a more complex case is simulated, involving the water-cooled nozzle of a rocket-based combined cycle thruster. This case employs all three models, fully coupled. The calculated temperatures in the nozzle wall and at the cooling channel outlet are compared with experimental data and are in reasonably close agreement.
机译:展示了涉及详细物理模型的实际几何形状的多学科模拟的可行性。具体地,三维化学反应流体流动求解器与包括冷却通道的固相传热求解器耦合。液相和固相模型均采用控制方程的积分形式和保守形式,并通过两个有限体积数值方案进行离散化。为了使热通量保持一致,在固体和流体区域之间的界面处开发了一种特殊的算法。固体材料的物理和热性能可能取决于温度,并且由于采用了多块网格化策略,因此可以在域的不同部分使用不同的材料。冷却通道模型是根据质量,动量和能量守恒定律而开发的,其中考虑了传热和摩擦的影响。详细介绍了模型(固体和流体,固体和冷却通道)的耦合。检查了热空气喷嘴测试用例,并通过可用的实验数据验证了模拟结果。最后,模拟了一个更复杂的情况,其中涉及基于火箭的联合循环推进器的水冷喷嘴。该案例采用了所有三种模型,完全耦合。将喷嘴壁和冷却通道出口处的计算温度与实验数据进行比较,并在相当接近的范围内。

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