LOSS OF LIFT DUE TO THICKNESS FOR LOW-ASPECT-RATIO WINGS IN INCOMPRESSIBLE-FLOW

被引:1
作者
DODBELE, SS [1 ]
PLOTKIN, A [1 ]
机构
[1] SAN DIEGO STATE UNIV,DEPT AEROSP ENGN & ENGN MECH,SAN DIEGO,CA 92182
关键词
D O I
10.1007/BF00127688
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
引用
收藏
页码:3 / 16
页数:14
相关论文
共 28 条
[1]  
Ashley H., 1965, AERODYNAMICS WINGS B
[2]   EXPERIMENTAL INVESTIGATION OF INFLUENCE OF EDGE SHAPE ON THE AERODYNAMIC CHARACTERISTICS OF LOW ASPECT RATIO WINGS AT LOW SPEEDS [J].
BARTLETT, GE ;
VIDAL, RJ .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (08) :517-&
[3]  
DODBELE SS, 1984, THESIS U MARYLAND
[4]  
DODBELE SS, 1985, AIAA851588
[5]   CALCULATION OF NONLINEAR SUBSONIC CHARACTERISTICS OF WINGS WITH THICKNESS AND CAMBER AT HIGH-INCIDENCE [J].
GORDON, R ;
ROM, J .
AIAA JOURNAL, 1985, 23 (06) :817-825
[6]  
HOEIJMAKERS HWM, 1983, AGARD CP, V342
[7]  
HUMMEL D, 1979, AGARD CP, V247
[8]  
JACQUET BN, 1948, NACA RM L8L29
[9]   3-DIMENSIONAL FLOW OVER WINGS WITH LEADING-EDGE VORTEX SEPARATION [J].
JOHNSON, FT ;
TINOCO, EN ;
LU, P ;
EPTON, MA .
AIAA JOURNAL, 1980, 18 (04) :367-380
[10]  
JOHNSON FT, 1979, AIAA790282