THE LIFT OF A DELTA-WING AT SUPERSONIC SPEEDS

被引：28

作者：

STEWART, HJ

机构：

来源：

QUARTERLY OF APPLIED MATHEMATICS | 1946年 / 4卷 / 03期

关键词：

D O I：

10.1090/qam/17096

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

引用

页码：246 / 254

页数：9

共 50 条

[1] WING VERTICAL POSITION EFFECTS ON LIFT FOR SUPERSONIC DELTA-WING MISSILES
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[2] ON THE LIFT OF A TRIANGULAR WING AT SUPERSONIC SPEEDS
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[3] NOTE ON THE LIFT OF A TRIANGULAR WING AT SUPERSONIC SPEEDS
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[4] THE EFFECT OF WING GEOMETRY ON LIFT AT SUPERSONIC SPEEDS
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[5] ANALYSIS OF FLOW AROUND A DELTA-WING WITH SUPERSONIC EDGES
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[6] THE YAWED DELTA WING AT INCIDENCE AT SUPERSONIC SPEEDS
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[7] EFFECT OF LEADING-EDGE SEPARATION ON THE LIFT OF A DELTA-WING
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[8] GENERALIZED AERODYNAMIC FORCES ON THE DELTA-WING WITH SUPERSONIC LEADING EDGES
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[9] Pressure sensitive paint measurements on a delta-wing in supersonic flow
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[10] FULL-POTENTIAL ANALYSIS OF A SUPERSONIC DELTA-WING BODY
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