Visualization of Shock Wave Phenomenon around a Sharp Cone Model at Hypersonic Mach Number in a Shock Tunnel using High Speed Schlieren Facility

Visualization of Shock Wave Phenomenon around a Sharp Cone Model at Hypersonic Mach Number in a Shock Tunnel using High Speed Schlieren Facility

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The flow field around a Sharp cone model configuration has been investigated by means of Schlieren facility in hypersonic shock tunnel. The time dependent evolution of flow around a cone of angle 11.38° with base radius of 150mm has been visualized for a flow Mach number M = 6.5. Experiments have...

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Bibliographic Details
Main Authors:	M. Saiprakash, C. Senthil Kumar, G. K. Sunil, S. P. Rampratap, V. Shanmugam, G. Balu
Format:	Article
Language:	English
Published:	Isfahan University of Technology 2019-01-01
Series:	Journal of Applied Fluid Mechanics
Subjects:	Sharp Cone model; High speed Schlieren facility; Hypersonic shock; Tunnel; Shock layer thickness.
Online Access:	http://jafmonline.net/JournalArchive/download?file_ID=48430&issue_ID=255

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