Experimental studies of laminar separated flows induced by shock wave/boundary layer and shock/shock interaction in hypersonic flows for CFD validation

2000 ◽  
Author(s):  
Michael Holden
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Experimental Studies ◽  
Hypersonic Flows ◽  
Separated Flows ◽  
Shock Interaction ◽  
Cfd Validation ◽  
Wave Boundary Layer ◽  
Wave Boundary

scholarly journals CFD Validation Experiment of a Mach 2.5 Axisymmetric Shock-Wave/Boundary-Layer Interaction

2015 ◽  
Author(s):  
David O. Davis
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Region Of Interest ◽  
Two Dimensional ◽  
Cfd Validation ◽  
Layer Interaction ◽  
Wave Boundary Layer ◽  
Validation Experiment ◽  
Boundary Layer Interaction ◽  
Wave Boundary

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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