AN ASYMPTOTIC SOLUTION FOR CENTRE OF A ROLLED-UP CONICAL VORTEX SHEET IN COMPRESSIBLE FLOW

被引:3
作者
BROWN, SN
MANGLER, KW
机构
来源
AERONAUTICAL QUARTERLY | 1967年 / 18卷
关键词
D O I
10.1017/S0001925900004339
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:354 / &
相关论文
共 10 条
[1]   COMPRESSIBLE INVISCID LEADING-EDGE VORTEX [J].
BROWN, SN .
JOURNAL OF FLUID MECHANICS, 1965, 22 :17-&
[2]   A THEORY FOR THE CORE OF A LEADING-EDGE VORTEX [J].
HALL, MG .
JOURNAL OF FLUID MECHANICS, 1961, 11 (02) :209-228
[3]   FLOW FIELD NEAR CENTRE OF A ROLLED-UP VORTEX SHEET [J].
MANGLER, KW ;
WEBER, J .
JOURNAL OF FLUID MECHANICS, 1967, 30 :177-&
[4]   A THEORY OF THE FLOW PAST A SLENDER DELTA WING WITH LEADING EDGE SEPARATION [J].
MANGLER, KW ;
SMITH, JHB .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1959, 251 (1265) :200-217
[5]  
MANGLER KW, 1967, RAE67029 TECH REP
[6]  
MANGLER KW, 1965, Z ANGEWANDTE MATHEMA, V45, P165
[7]  
MANGLER KW, RAE66324 TECH REP
[8]  
MICHAEL WH, 1955, TN3472 NACA
[9]  
SMITH JHB, 1966, RAE66070 TECH REP
[10]   THE INNER VISCOUS SOLUTION FOR THE CORE OF A LEADING-EDGE VORTEX [J].
STEWARTSON, K ;
HALL, MG .
JOURNAL OF FLUID MECHANICS, 1963, 15 (02) :306-318