Affiliation:
1. Techspace Aero, Safran Group, Route de Liers 121, B-4041 Milmort, Belgium
2. FNRS Research Fellow
3. Turbomachinery Group, University of Liège, Chemin des Chevreuils 1, B-4000 Liège, Belgium
Abstract
This paper presents a throughflow analysis tool developed in the context of the average-passage flow model elaborated by Adamczyk. The Adamczyk’s flow model describes the 3D time-averaged flow field within a blade row passage. The set of equations that governs this flow field is obtained by performing a Reynolds averaging, a time averaging, and a passage-to-passage averaging on the Navier–Stokes equations. The throughflow level of approximation is obtained by performing an additional circumferential averaging on the 3D average-passage flow. The resulting set of equations is similar to the 2D axisymmetric Navier–Stokes equations, but additional terms resulting from the averages show up: blade forces, blade blockage factor, Reynolds stresses, deterministic stresses, passage-to-passage stresses, and circumferential stresses. This set of equations represents the ultimate throughflow model provided that all stresses and blade forces can be modeled. The relative importance of these additional terms is studied in the present contribution. The stresses and the blade forces are determined from 3D steady and unsteady databases (a low-speed compressor stage and a transonic turbine stage) and incorporated in a throughflow model based on the axisymmetric Navier–Stokes equations. A good agreement between the throughflow solution and the averaged 3D results is obtained. These results are also compared to those obtained with a more “classical” throughflow approach based on a Navier–Stokes formulation for the endwall losses, correlations for profile losses, and a simple radial mixing model assuming turbulent diffusion.
Reference23 articles.
1. Computational Fluid Dynamics for Turbomachinery Design;Denton;Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci.
2. Semiviscous Method for Compressor Performance Prediction;Attia;J. Propul. Power
3. The Prediction of 3-D Transonnic Flow in Turbomachinery Using a Combined Throughflow and Blade-to-Blade Time Marching Method;Spurr;Int. J. Heat Fluid Flow
4. Baralon, S.
, 2000, “On Multistage Analysis of Transonic Compressors: From Axisymmetric Throughflow Time Marching to Unsteady Three Dimensional Methods,” Ph.D. thesis, Chalmers University of Technology, Gothenburg, Sweden
5. Sturmayr, A.
, 2004, “Evolution of a 3-D Structured Navier-Stokes Solver Towards Advanced Turbomachinery Applications,” Ph.D. thesis, Vrije Universiteit Brussel, Brussels, Belgium.
Cited by
10 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献