Satheesh, K and Jagadeesh, G (2009) Measurement of shock stand-off distance on a 120 degrees blunt cone model at hypersonic Mach number in Argon. In: 26th International Symposium on Shock Waves, JUL 15-20, 2007, Gottingen.
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The flow around a 120 degrees blunt cone model with a base radius of 60mm has been visualised at Mach 14.8 and 9.1 using argon as the test gas, at the newly established high speed schlieren facility in the IISc hypersonic shock tunnel HST2. The experimental shock stand off distance around the blunt cone is compared with that obtained using a commercial CFD package. The computed values of shock stand off distance of the blunt cone is found to agree reasonably well with the experimental data.
|Item Type:||Conference Paper|
|Additional Information:||Copyright of this article belongs to Springer.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||07 Jun 2010 09:05|
|Last Modified:||19 Sep 2010 05:56|
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