Numerical simulation of flows around axisymmetric inlet with bleed regions

被引：6

作者：

Kwak, Einkeun ^{[1
]}

Lee, Hyungro ^{[1
]}

Lee, Seungsoo ^{[1
]}

机构：

[1] Inha Univ, Dept Aerosp Engn, Inchon 402751, South Korea

来源：

JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY | 2010年 / 24卷 / 12期

关键词：

Axisymmetric inlet; Bleed boundary condition; Numerical simulation; RANS equations; Two-equation turbulence models; TURBULENCE MODELS;

D O I：

10.1007/s12206-010-0927-x

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

A numerical simulation of flows in an axisymmetric supersonic inlet with bleed regions is performed. An existing code which solves the Reynolds Averaged Navier-Stokes equations and the two-equation turbulence model equations is converted into an axisymmetric code. In addition, a bleed boundary condition model has been applied to the code. In this paper, the modified code is validated by comparing numerical results against experimental data and other computational results for flows on a bump and over an oblique shock with bleed region. Using the code, numerical simulation is performed for the flows in an inlet with multiple bleed regions.

引用

页码：2487 / 2495

页数：9