EXPERIMENTAL WORK ON THE AERODYNAMICS OF INTEGRATED SLENDER WINGS FOR SUPERSONIC FLIGHT

被引：2

作者：

SQUIRE, LC ^{[1
]}

机构：

[1] UNIV CAMBRIDGE,DEPT ENGN,CAMBRIDGE CB2 1PZ,ENGLAND

来源：

PROGRESS IN AEROSPACE SCIENCES | 1981年 / 20卷 / 01期

关键词：

D O I：

10.1016/0376-0421(81)90002-6

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1 / 96

页数：96

共 50 条

[1] Aerodynamics of Supersonic Flight
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[2] AERODYNAMICS OF THIN QUADRILATERAL WINGS AT SUPERSONIC SPEEDS
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[3] AERODYNAMICS OF WINGS IN SUPERSONIC SHEAR-FLOW
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[4] AERODYNAMICS OF SLENDER ROLLING WINGS AT INCIDENCE IN SEPARATED FLOW
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[5] AERODYNAMICS OF SLENDER LIFTING SURFACE IN ACCELERATED FLIGHT
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[8] Aerodynamics of Morphing Wings in Flapping and Gliding Flight
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[9] Aerodynamics of maneuvering slender wings with leading-edge separation
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[10] Unsteady aerodynamics of flapping bionic eagle wings in forward flight: An experimental and numerical study
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