COMPUTATION OF 3-DIMENSIONAL VISCOUS LINEAR CASCADE FLOWS

被引：11

作者：

CHOI, D

KNIGHT, CJ

机构：

[1] Avco Research Lab Inc, United States

来源：

AIAA JOURNAL | 1988年 / 26卷 / 12期

关键词：

Fluid Dynamics--Computation - Heat Transfer--Prediction - Mathematical Techniques--Numerical Methods - Viscosity;

D O I：

10.2514/3.10066

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A three-dimensional viscous cascade code has been developed for linear cascades with flat, parallel endwalls. It employs scalar implicit approximate factorization, a finite-volume formulation, second-order upwind differencing, and a two-equation q-ω turbulence model based on integration to the wall. A special form of the thin-layer approximation for the compressible Navier-Stokes equations is used which gives accurate skin-friction predictions on highly skewed meshes, now based on sheared H-grids. This code has been validated by considering three-dimensional viscous flows in L.S. Langston's large-scale turbine blade geometry. This validation includes three-dimensional heat-transfer predictions. Agreement with experiment is quite good.

引用

页码：1477 / 1482

页数：6

共 6 条

[1]

COAKLEY TJ, 1983, AIAA831693 PAP

[2]

GRAZIANI RA, 1980, ASME, V102, P257

[3]

KNIGHT CJ, 1987, AIAA872150 PAP

[4]

KOPPER FC, 1981, NASA CR165567 HIGH P

[5] 3-DIMENSIONAL FLOW WITHIN A TURBINE CASCADE PASSAGE [J].

LANGSTON, LS ;

NICE, ML ;

HOOPER, RM .

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[6] Approximate Riemann solvers, parameter vectors, and difference schemes (Reprinted from the Journal of Computational Physics, vol 43, pg 357-372, 1981) [J].

Roe, PL .

JOURNAL OF COMPUTATIONAL PHYSICS, 1997, 135 (02) :250-258

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