CONTROLLING THE SPACING OF STREAMWISE VORTICES ON CONCAVE WALLS

被引:13
作者
MYOSE, RY
BLACKWELDER, RF
机构
[1] University of Southern California, Department of Aerospace Engineering, Los Angeles, CA
关键词
D O I
10.2514/3.10816
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The wavelength of Gortler streamwise vortices was changed by a factor of three by varying the amount of tunnel side wall boundary-layer removal just upstream of the concave wall test section's leading edge. Nondimensional wavelengths in the range 215 less-than-or-equal-to LAMBDA less-than-or-equal-to 900 were achieved with the larger wavelengths resulting from increased suction. The minimum wavelength compares well with the maximum amplification curve based on past theoretical studies. Low-speed streaks appeared to merge with other low-speed streaks or were weakened to the point of disappearing as the suction level was increased. The downstream location of secondary instability onset changed with variation in suction level and/or wavelength. The Gortler number and amplification factor for secondary instability onset, however, was approximately independent of suction level and/or wavelength.
引用
收藏
页码:1901 / 1905
页数:5
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