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Towards Efficient CFD-Simulations of Engine Like Turbine Guide Vane Film Cooling

机译:迈向高效的CFD模拟发动机如涡轮导向叶片冷却

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It is well known that the efficiency of a gas turbine can be increased by using higher combustion temperatures and that this demands improved cooling. This study focuses on strategies to decrease the turnaround time for numerical predictions of film cooling while keeping the ability to resolve details of the flow. Simulations have been carried out for a real vane geometry at close to engine-like conditions and results are compared with corresponding experiments. The investigation includes an un-cooled situation for aerodynamic validation and to determine baseline heat transfer coefficent. Simulations and experiments of film effectiveness and heat transfer coefficient and their dependence of blowing ratio are investigated.
机译:众所周知,通过使用更高的燃烧温度可以提高燃气轮机的效率,并且这需要改善的冷却。这项研究的重点是减少薄膜冷却数值预测的周转时间,同时保持解决流细节的能力的策略。已经在接近发动机的条件下对真实叶片几何形状进行了仿真,并将结果与​​相应的实验进行了比较。研究包括未冷却的情况,以进行空气动力学验证并确定基线传热系数。研究了薄膜有效性和传热系数及其与吹塑比的关系的模拟和实验。

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