Publication Date:
2019-07-13
Description:
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.
Keywords:
Fluid Mechanics and Thermodynamics
Type:
NASA/TM-2015-218841
,
AJK2015-06342
,
GRC-E-DAA-TN23467
,
Joint Fluids Engineering Conference 2015; Jul 26, 2015 - Jul 31, 2015; Seoul; Korea, Republic of
Format:
application/pdf