Efficient Edge-Based Rotor/Stator Interaction Method

被引：71

作者：

Burgos, Manuel A. ^{[1
]}

Contreras, Jesus ^{[2
]}

Corral, Roque ^{[2
]}

机构：

[1] Univ Politecn Cartagena, Dept Fluid Dynam, Murcia 30006, Spain

[2] Ind Turbopropulsores SA, Technol & Methods Dept, Madrid 28830, Spain

来源：

AIAA JOURNAL | 2011年 / 49卷 / 01期

关键词：

TURBOMACHINERY FLOWS; SOLVERS;

D O I：

10.2514/1.44512

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A method to address the rotor/stator interaction problem on an edge-based Reynolds-averaged Navier-Stokes solver is presented. The implementation of the phase-lagged boundary conditions and a new original conservative discretization of the sliding plane in an unstructured solver is discussed in detail. The numerical method is implicit in time, and convergence is accelerated using a multigrid technique where the coarser grids are obtained by agglomeration. Results of the present method are compared with the experimental results obtained at the National Aerospace Laboratory (The Netherlands) for a subsonic fan.

引用

页码：19 / 31

页数：13

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