Hypersonic aerodynamic heating prediction using weighted essentially nonoscillatory schemes

被引：3

作者：

Lee, TK ^{[1
]}

Zhong, XL

Gong, L

Quinn, R

机构：

[1] Univ Calif Los Angeles, Dept Mech & Aerosp Engn, Los Angeles, CA 90095 USA

[2] NASA, Dryden Flight Res Ctr, Engn & Tech Serv, Edwards AFB, CA 93523 USA

[3] Analyt Serv & Mat Inc, Aerostruct Branch, Hampton, VA 23666 USA

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 2003年 / 40卷 / 02期

关键词：

D O I：

10.2514/2.3946

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The aerodynamic heating prediction around hypersonic vehicles was done. The accurate calculation of surface heating rates on hypersonic vehicles was found to be dependent on an accurate inviscid computational fluid dynamics (CFD) numerical solution of the mean aerodynamic flow properties. The weighted essentially nonoscillatory schemes for aerodynamic heating prediction were presented.

引用

页码：294 / 298

页数：5

共 13 条

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