IMPROVED CALCULATIONS OF LEADING-EDGE SEPARATION FROM SLENDER THIN DELTA WINGS

被引：56

作者：

SMITH, JHB

机构：

来源：

PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES | 1968年 / 306卷 / 1484期

关键词：

D O I：

10.1098/rspa.1968.0138

中图分类号：

O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];

学科分类号：

07 ; 0710 ; 09 ;

摘要：

引用

页码：67 / &

共 21 条

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[5] COMPRESSIBLE INVISCID LEADING-EDGE VORTEX
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[8] A THEORY FOR THE CORE OF A LEADING-EDGE VORTEX
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[J]. JOURNAL OF FLUID MECHANICS, 1961, 11 (02) : 209 - 228
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[10] LEGENDRE R, 1966, PROGRESS AERONAUTICA, V7