CFD VALIDATION EXPERIMENT OF A MACH 2.5 AXISYMMETRIC SHOCK-WAVE/BOUNDARY-LAYER INTERACTION

被引：0
|
作者：
Davis, David O. [1 ]
机构：
[1] NASA, Glenn Res Ctr, Cleveland, OH USA
来源：
PROCEEDINGS OF THE ASME/JSME/KSME JOINT FLUIDS ENGINEERING CONFERENCE, 2015, VOL 1 | 2015年
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D O I：
暂无
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
Preliminary results of an experimental investigation of a Mach 2.5 two-dimensional axisymmetric shock-wave/boundary-layer interaction (SWBLI) are presented. The purpose of the investigation is to create a SWBLI dataset specifically for CFD validation purposes. Presented herein are the details of the facility and preliminary measurements characterizing the facility and interaction region. These results will serve to define the region of interest where more detailed mean and turbulence measurements will be made.
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页数：11
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