3-LAYER INTERACTIVE METHOD FOR COMPUTING SUPERSONIC LAMINAR SEPARATED FLOWS

被引:1
作者
BRANDEIS, J [1 ]
ROM, J [1 ]
机构
[1] TECHNION ISRAEL INST TECHNOL,DEPT AERONAUT ENGN,HAIFA,ISRAEL
关键词
D O I
10.2514/3.7726
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:1320 / 1327
页数:8
相关论文
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