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Numerical Validations of Secondary Flows and Loss Development Downstream of a Highly Loaded Low Pressure Turbine Outlet Guide Vane Cascade

机译:高负载低压涡轮机出口导向叶片级联下游二次流量和损失开发的数值验证

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In this paper 3D numerical simulations of turbulent incompressible flows are validated against experimental data from the linear low pressure turbine/outlet guide vane (LPT/OGV) cascade at Chalmers in Sweden. The validation focuses on the secondary flow-fields and loss developments downstream of a highly loaded OGV. The numerical simulations are performed for the same inlet conditions as in the test-facility with engine-like properties in terms of Reynolds number, boundary-layer thickness and inlet flow angles with the goal to validate how accurately and reliably the secondary flow fields and losses for both on- and off-design conditions can be predicted for OGV's. Results from three different turbulence models as implemented in FLUENT, k-εRealizable, kω-SST and the RSM are validated against detailed measurements. From these results it can be concluded that the RSM model predicts both the secondary flow field and the losses most accurately.
机译:在本文中,3D湍流不可压缩流量的数值模拟验证了来自瑞典Chalmers的线性低压涡轮/出口导向叶片(LPT / OGV)级联的实验数据。验证侧重于高负载OGV下游的二次流场和损失开发。在雷诺数方面,在测试设施中,对具有发动机的性质的相同入口条件执行数值模拟,边界层厚度和入口流动角度,其中目标是验证次要流场和损耗的准确性和可靠性对于OGV来说,可以预测开启和非设计条件。在流利,K-ε1aalizable,KΩ-SST和RSM中实现的三种不同湍流模型的结果是以详细测量验证的。从这些结果可以得出结论,RSM模型最准确地预测二次流场和损耗。

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