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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Bibliographic Details
Title: Visualization of Shock Wave Phenomenon around a Sharp Cone Model at Hypersonic Mach Number in a Shock Tunnel using High Speed Schlieren Facility.
Authors: Saiprakash, M.1, iamsaiaero@gmail.com, SenthilKumar, C.1, Sunil, G. K.2, Rampratap, S. P.2, Shanmugam, V.2, Balu, G.2
Source: Journal of Applied Fluid Mechanics; 2019, Vol. 12 Issue 2, p461-468, 8p
Database: Applied Science & Technology Source
Description
ISSN:17353572
DOI:10.29252/jafm.12.02.29250