Near exit plane effects caused by primary and primary-plus-secondary tabs

被引:23
作者
Bohl, DG [1 ]
Foss, JF [1 ]
机构
[1] Michigan State Univ, Dept Mech Engn, E Lansing, MI 48824 USA
关键词
D O I
10.2514/2.713
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Triangular-shaped tabs, attached to the separation lip of a nozzle, have been shown to provide substantial increases in the convective transport-mixing in a jet's near field. Detailed information is reported on the basic features of such tab flows made available by 1) the large-scale tab and 2) the finely resolved pressure/velocity measurements, Secondary tabs Here placed next to, and pointed away from, the primary tab; the motivation was to enhance the outward directed flow from the jet's core region. The strong mixing enhancement, provided by these optimally oriented (pitch angle = 40 deg) secondary tabs, is detailed.
引用
收藏
页码:192 / 201
页数:10
相关论文
共 16 条
[1]  
Ahuja K., 1989, 2 SHEAR FLOW C, DOI DOI 10.2514/MSFC89
[2]  
BOHL D, 1997, CR97206296 NASA
[3]  
Bohl D. G., 1996, 960545 AIAA
[4]  
BOHL DG, 1995, 950102 AIA
[5]   DISTORTION OF A JET BY TABS [J].
BRADBURY, LJS ;
KHADEM, AH .
JOURNAL OF FLUID MECHANICS, 1975, 70 (AUG26) :801-813
[6]  
BRUNS JM, 1991, 8 S TURB SHEAR FLOWS
[7]   2-DIMENSIONAL CONVECTION FROM HEATED WIRES AT LOW REYNOLDS NUMBERS [J].
COLLIS, DC ;
WILLIAMS, MJ .
JOURNAL OF FLUID MECHANICS, 1959, 6 (03) :357-384
[8]  
FOSS J, 1996, HDB FLUID DYNAMICS F, V2, P1064
[9]   AN EXPERIMENTAL-STUDY OF ORGANIZED MOTIONS IN THE TURBULENT PLANE MIXING LAYER [J].
HUSSAIN, AKMF ;
ZAMAN, KBMQ .
JOURNAL OF FLUID MECHANICS, 1985, 159 (OCT) :85-104
[10]  
LIEPMANN HW, 1947, 1257 NACA