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    CFD Validation Experiment of a Mach 2.5 Axisymmetric Shock-Wave Boundary-Layer Interaction (2015)
    In:  CASI
    Details
    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. The 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: AJK2015-06342 , GRC-E-DAA-TN23733 , 2015 AJK Fluids Engineering Division Summer Meeting; Jul 26, 2015 - Jul 31, 2015; Seoul; Korea, Republic of
    Format: application/pdf
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