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Calculation of three-dimensional, viscous flow through turbomachinery blade passages by parabolic marching

机译:通过抛物线行进计算通过涡轮机叶片通道的三维粘性流

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摘要

The three-dimensional compressible Navier-Stokes equations are formulated in a rotating coordinate system, so as to include centrifugal and Coriolis forces. The equations are parabolized by using a previously calculated inviscid static pressure field. The thin layer Navier-Stokes approximation, which neglects streamwise diffusion, is used. A body-fitted coordinate system is used. The streamwise momentum equation is uncoupled from the cross-stream momentum equation by using contravariant momentum components, and then using the contravariant velocity components as primary unknowns. To reduce problems with small separated regions, the Reyhner and Flugge-Lotz approximation is used. The energy equation is included to allow for calculation of heat transfer. The flow may be laminar, or a simple eddy-viscosity turbulence may be used. A number of curved ducts and an axial stator were analyzed, including cases for which experimental data are available.
机译:三维可压缩的Navier-Stokes方程在旋转坐标系中表示,以便包括离心力和科里奥利力。通过使用先前计算的无形静态压力场将方程式抛物线化。使用了忽略流向扩散的薄层Navier-Stokes近似。使用适合身体的坐标系。通过使用协变动量分量,然后将协变速度分量作为主要未知量,将流向动量方程与横流动量方程解耦。为了减少较小的分离区域的问题,使用了Reyhner和Flugge-Lotz近似。包含了能量方程式,以便计算传热。流动可以是层流的,或者可以使用简单的涡流-粘性湍流。分析了许多弯曲导管和轴向定子,包括可获得实验数据的情况。

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    Katsanis, T.;

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  • 年度 1985
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