NUMERICAL-SOLUTION OF 2-DIMENSIONAL TURBULENT BLUNT BODY FLOWS WITH AN IMPINGING SHOCK

被引:4
作者
TANNEHILL, JC
VIGNERON, YC
RAKICH, JV
机构
[1] IOWA STATE UNIV SCI & TECHNOL,ENGN RES INST,AMES,IA 50011
[2] NASA,AMES RES CTR,DEPT AEROSP ENGN,MOFFETT FIELD,CA 94035
关键词
D O I
10.2514/3.61309
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An implicit finite-difference method has been developed to compute two-dimensional, turbulent, blunt-body flows with an impinging shock wave. The complete timeaveraged Navier-Stokes equations are solved with algebraic eddy viscosity and turbulent Prandtl number models employed for shear stress and heat flux. The irregular-shaped bow shock is treated as a discontinuity across which the Rankine-Hugoniot equations are applied. A Type III turbulent shock interference flowfield has been computed and the numerical results compare favorably with existing experimental data. © 1979 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.
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页码:1289 / 1290
页数:2
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