Effect of Varying Ramp Angle and Leading-Edge Bluntness on the Behavior of Ramp Induced Shock Wave over Triple Ramped Cone Flare Configuration at Hypersonic Speed

Numerical simulation results are presented to show the effect of ramp angle variations and leading-edge bluntness on the flow around triple ramped cone flare in hypersonic flow. This study investigates the changes associated with shock wave boundary layer interaction due to ramp induced flow breakdo...

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Bibliographic Details
Published inInternational journal of recent technology and engineering Vol. 8; no. 3; pp. 8127 - 8138
Main Authors Sundarraj, Karthik, Guven, Ugur, Kulkarni, P S, Prakash, Om, Pawar R, Ganesh
Format Journal Article
LanguageEnglish
Published 30.09.2019
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