EFFECTS OF YAW ON CONICAL WINGS AT HIGH SUPERSONIC SPEEDS

被引：11

作者：

HILLIER, R

机构：

来源：

AERONAUTICAL QUARTERLY | 1970年 / 21卷

关键词：

D O I：

10.1017/S0001925900005394

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：199 / &

共 50 条

[1] DYNAMIC DERIVATIVES IN YAW AND SIDESLIP OF THIN WINGS AT SUPERSONIC SPEEDS
GOODMAN, TR
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (04): : 357 - 367
[2] CALCULATED PRESSURE DISTRIBUTIONS AND SHOCK SHAPES ON THICK CONICAL WINGS AT HIGH SUPERSONIC SPEEDS
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[3] EFFECTS OF YAW ON A GOTHIC WING AT SUPERSONIC SPEEDS
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[4] WAVE DRAG OF WINGS AT SUPERSONIC SPEEDS
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[5] AERODYNAMICS OF THIN QUADRILATERAL WINGS AT SUPERSONIC SPEEDS
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[6] AERODYNAMIC CHARACTERISTICS OF RECTANGULAR WINGS AT SUPERSONIC SPEEDS
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[7] EFFECT OF YAW ON SUPERSONIC AND HYPERSONIC FLOW OVER DELTA WINGS
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[8] AERODYNAMIC PERFORMANCE OF DELTA-WINGS AT SUPERSONIC SPEEDS
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[9] DRAG DUE TO LIFT FOR DELTA WINGS AT SUPERSONIC SPEEDS
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JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (12): : 919 - 920
[10] THE WARPING OF TRIANGULAR WINGS FOR MINIMUM DRAG AT SUPERSONIC SPEEDS
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