Linear approximation for supersonic flow past a delta wing

被引：5

作者：

Chen, SX ^{[1
]}

机构：

[1] Fudan Univ, Inst Math, Shanghai 200433, Peoples R China

来源：

ARCHIVE FOR RATIONAL MECHANICS AND ANALYSIS | 1997年 / 140卷 / 04期

关键词：

Linear Approximation; Supersonic Flow;

D O I：

10.1007/s002050050069

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

[No abstract available]

引用

页码：319 / 333

页数：15

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