2010
DOI: 10.2322/jjsass.58.123
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Reattaching Flow Visualization by Means of Glow Spark in Hypersonic Shock-Wave/Boundary-Layer Interaction

Abstract: :The purpose of this study was to examine the structure of reattaching boundary layers downstream of a quasi-two-dimensional compression corner in a gun tunnel at Mach number 10 using a glow spark technique. An analytical model predicted well a location of a high aerodynamic heating region in laminar reattaching boundary layers. An indication of presence of Görtler vortices was found; the vortices may play an important role in the transition. Furthermore, the flow was unsteady and accompanied by a shock wave r… Show more

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