THE WAVE DRAG AT ZERO LIFT OF SLENDER DELTA WINGS AND SIMILAR CONFIGURATIONS

被引：4

作者：

LIGHTHILL, MJ

机构：

来源：

关键词：

D O I：

10.1017/S0022112056000196

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：337 / 348

页数：12

共 50 条

[1] WAVE DRAG OF WINGS AT ZERO LIFT IN INVISCID AIRFLOW.
Anon
Engineering Sciences Data Unit, Data Items, 1975,
[2] SUPERSONIC FLOW PAST SLENDER POINTED WINGS WITH SIMILAR CROSS SECTIONS AT ZERO LIFT
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[3] LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
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[4] DRAG DUE TO LIFT FOR DELTA WINGS AT SUPERSONIC SPEEDS
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[5] MAXIMUM LIFT ON SLENDER WINGS
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[6] THEORETICAL PRESSURE DISTRIBUTION AT ZERO LIFT AT SUPERSONIC SPEEDS FOR SLENDER DELTA-WINGS HAVING FUSELAGES OF CIRCULAR CROSS SECTION
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[7] LIFT EFFECTIVENESS OF SLENDER WINGS ON CYLINDRICAL BODIES
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[8] NOTE ON THE WAVE DRAGS OF UNTAPERED WINGS WITH STREAMWISE TIPS AT ZERO LIFT
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[9] Lift and drag characteristics of rotary and flapping wings
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[10] ON LIFT OF VERY SLENDER-WINGS AT LOW SPEED
EHRLICH, E
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