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Visualization of incipient flow separation condition on hypersonic shock-boundary layer interaction

DSpace at IIT Bombay

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Title Visualization of incipient flow separation condition on hypersonic shock-boundary layer interaction
 
Creator TALSANIYA, HM
MENEZES, V
NITHIN, B
KULKARNI, V
 
Subject Shock
Boundary layer
Hypersonic
Viscous interactions
 
Description This article presents an investigation on a correlation relevant to flow separation during shock wave-boundary layer interaction in a hypersonic flow. The study includes experimental as well as numerical components. The hypersonic shock-boundary layer interactions were visualized to gauge the extent of flow separation on a flat plate on external shock impingement. The pressure in the vicinity of shock impingement was measured. Through visualized images, the applicability of the correlation to flow separation due to externally impinged shock waves was analyzed. Qualitative numerical simulations were carried out to have an insight into the hypersonic shock-boundary layer interactions.
 
Publisher SPRINGER
 
Date 2016-01-14T12:44:00Z
2016-01-14T12:44:00Z
2015
 
Type Article
 
Identifier JOURNAL OF VISUALIZATION, 18(4)611-618
1343-8875
1875-8975
http://dx.doi.org/10.1007/s12650-015-0274-1
http://dspace.library.iitb.ac.in/jspui/handle/100/17528
 
Language en