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LARGE EDDY SIMULATION OF FILM COOLING FLOW ABOVE A FLAT PLATE FROM INCLINED CYLINDRICAL HOLES

机译:倾斜圆柱孔上平板的薄膜冷却流动的大涡模拟

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摘要

Large Eddy Simulation of a realistic film cooling configuration is performed, consisting of a large plenum feeding a periodic array of short film cooling holes with length to diameter ratio L/d = 3.5. Film cooling jets are issued at 35 degrees into the turbulent crossflow boundary layer above the flat surface. Time-averaged flowfield is analyzed to reveal steady and unsteady structures occurring as a result of plenum-jet-crossflow interactions. Among these structures are the flow separation inside the film-hole, reverse flow zone right behind the jet injection and the counter-rotating vortex pair in the wake of the jet. All of these structures influence the wall temperature distribution and have a negative effect on film cooling effectiveness.
机译:大涡流对实际的薄膜冷却配置进行仿真,该过程由一个大增压室供入,周期性排列的短薄膜冷却孔阵列的长径比为L / d = 3.5。薄膜冷却射流以35度角射入平坦表面上方的湍流横流边界层。分析了时间平均流场,以揭示由于增压-射流-横流相互作用而产生的稳定和不稳定结构。在这些结构中,有薄膜孔内部的流动分离,紧接在射流注入之后的反向流动区以及在射流之后产生的反向旋转涡流对。所有这些结构都会影响壁温分布,并对薄膜冷却效果产生负面影响。

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