CALCULATION OF SYMMETRIC VORTEX SEPARATION AFFECTING SUBSONIC BODIES AT HIGH-INCIDENCE

被引:8
作者
ALMOSNINO, D
ROM, J
机构
[1] TECHNION ISRAEL INST TECHNOL,DEPT AERONAUT ENGN,HAIFA,ISRAEL
[2] TECHNION ISRAEL INST TECHNOL,LADY DAVIS CHAIR EXPTL AERODYNAM,HAIFA,ISRAEL
关键词
D O I
10.2514/3.8086
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:398 / 406
页数:9
相关论文
共 38 条
[1]  
ALMOSNINO D, 1978, ISRAEL J TECHNOL, V16, P132
[2]  
ANGELUCCI SB, 1971, J AIRCRAFT, V8, P959, DOI DOI 10.2514/3.44317
[3]  
ANGELUCCI SB, 1973, AIAA73104 PAP
[4]   APPLICATION OF THE VORTEX-LATTICE TECHNIQUE TO ARBITRARY BODIES [J].
ASFAR, KR ;
MOOK, DT ;
NAYFEH, AH .
JOURNAL OF AIRCRAFT, 1979, 16 (07) :421-424
[5]  
ATTA E, 1978, AIAA781206 PAP
[6]  
CLARK WC, 1976, AIAA7665 PAP
[7]  
CLARK WH, 1972, AIAA72968 PAP
[8]  
CLARK WH, 1977, AIAA771154 PAP
[9]  
DEFFENBAUGH FD, 1976, AIAA76364 PAP
[10]   APPROXIMATE METHOD FOR ESTIMATING WAKE VORTEX STRENGTH [J].
FIDLER, JE .
AIAA JOURNAL, 1974, 12 (05) :633-635