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稀薄过渡流区横向喷流干扰效应数值模拟研究

梁杰 阎超 李志辉 李绪国

空气动力学学报2013,Vol.31Issue(1):27-33,7.
空气动力学学报2013,Vol.31Issue(1):27-33,7.DOI:10.7638/kqdlxxb20130105

稀薄过渡流区横向喷流干扰效应数值模拟研究

Numerical investigation of lateral jet interaction effects in rarefied transition flow regime

梁杰 1阎超 2李志辉 1李绪国2

作者信息

  • 1. 北京航空航天大学航空科学与工程学院,北京 100191
  • 2. 中国空气动力研究与发展中心,四川绵阳 621000
  • 折叠

摘要

Abstract

A parallel DSMC method is presented for accuratly predicting the effects of lateral jet interaction with rarefied atmosphere of transition flow.A hybrid grid structure with Cartesian coordinate meshes and surface unstructured triangular cells is developed with collision cells adaptation and used in the DSMC computation.A static random load balancing technique is applied in the parallel DSMC code using the MPI parallel environment.For the computation of lateral jet interaction of three-dimensional plat plate model with different pressure ratios, the results of surface separation distance show good agreement with low density wind tunnel experiment to validate the DSMC algorithm.The supersonic and hypersonic RCS jet interaction with hypersonic rarefied incoming flow on a slender blunt double-cone in rarefied transition flow regime are investigated.The impacts of flight altitude, free stream velocity, angle of attack and jet thrust on plume-atmosphere interaction flow fields and aerodynamic properties are numerically analyzed.The influences of parameter distributions with uniform /non-uniform of nozzle exit on the seperation distance and votex structure near the jet are simulated in detail.

关键词

DSMC方法/网格自适应/并行算法/稀薄过渡流/喷流干扰

Key words

DSMC method/ Cartesian coordinate grid/ parallel algorithm/ rarefied transition flow/ jet interaction

分类

航空航天

引用本文复制引用

梁杰,阎超,李志辉,李绪国..稀薄过渡流区横向喷流干扰效应数值模拟研究[J].空气动力学学报,2013,31(1):27-33,7.

基金项目

国家自然科学基金(91016027),国防基础科研基金项目(51313030104) (91016027)

空气动力学学报

OA北大核心CSCDCSTPCD

0258-1825

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