首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.6 pt.A; 20070514-17; Montreal(CA) >Numerical Validations of Secondary Flows and Loss Development Downstream of a Highly Loaded Low Pressure Turbine Outlet Guide Vane Cascade
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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:高负荷低压涡轮出口导流叶片叶栅下游二次流动和损失形成的数值验证

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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-ε Realizable, 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:本文利用来自瑞典查尔默斯的线性低压涡轮/出口导流叶片(LPT / OGV)级联的实验数据验证了湍流不可压缩流的3D数值模拟。验证的重点是高负荷OGV下游的次级流场和损失发展。在与具有雷诺数,边界层厚度和进气流角的发动机类似特性的测试设施相同的进气条件下进行了数值模拟,目的是验证二次流场和损失的准确性和可靠性。可以预测OGV的设计和非设计条件。 FLUENT,k-εRealizable,kω-SST和RSM中实现的三种不同湍流模型的结果已针对详细测量进行了验证。从这些结果可以得出结论,RSM模型可以最准确地预测二次流场和损失。

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