Investigation of the calmed region behind a turbulent spot

被引:30
作者
Gostelow, JP
Walker, GJ
Solomon, WJ
Hong, G
Melwani, N
机构
[1] UNIV TASMANIA,HOBART,TAS 7001,AUSTRALIA
[2] UNIV TECHNOL SYDNEY,SYDNEY,NSW,AUSTRALIA
来源
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 1997年 / 119卷 / 04期
关键词
D O I
10.1115/1.2841191
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Measurements are presented of the calmed region behind triggered wave packets and turbulent spots under a controlled diffusion adverse pressure gradient in a wind tunnel. Similar measurements are also presented from the stator blades of an axial flow compressor, where turbulent spots are induced by the passing of rotor wakes. The purpose is to gain an appreciation of turbulent spot behavior under a strong adverse pressure gradient as a foundation for the more accurate modeling of spots and their environment in predictions of transitional boundary layer flows. Under an adverse pressure gradient the calmed region behind the spot is extensive; its interaction with the surrounding boundary layer is complex and is dependent on whether the surrounding natural boundary layer is laminar or turbulent. Some insights are gleaned concerning the behavior of the calmed region, which will subsequently be used in attempts to model the calmed region. Although these fundamental investigations of the calmed region have been extensive, much remains to be understood.
引用
收藏
页码:802 / 809
页数:8
相关论文
共 22 条
[1]  
BLACKWELDER RF, 1993, COMMUNICATION
[2]  
Cumpsty N. A., 1995, IGTI C HOUST TX
[3]  
GOSTELOW JP, 1996, ASME, V118, P737, DOI DOI 10.1115/1.2840929
[4]  
GOSTELOW JP, 1995, 952254 AIAA
[5]  
GOSTELOW JP, 1995, P 7 ISFV SEATTL FLOW, V7, P218
[6]  
GUTMARK E, 1987, EXP FLUIDS, V5, P217
[7]  
HALSTEAD DE, 1997, ASME, V119, P114, DOI DOI 10.1115/1.2841000
[8]  
HALSTEAD DE, 1997, ASME, V119, P426, DOI DOI 10.1115/1.2841142
[9]  
HALSTEAD DE, 1997, ASME, V119, P128, DOI DOI 10.1115/1.2841001
[10]  
HALSTEAD DE, 1997, ASME, V119, P225, DOI DOI 10.1115/1.2841105