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  1. No Access

    Article

    Impact of Shock Wave Boundary Layer Interaction on the Internal Flow and Performance of Scramjet Intake

    The investigation of shock wave boundary layer interaction (SWBLI) and the prediction of the associated flow field and surface property variation are essential elements in designing scramjet engine. Therefore,...

    A. A. Kane, R. K. Peetala, V. Kulkarni in Fluid Dynamics (2021)

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    Chapter and Conference Paper

    Effect of gas injection on drag and surface heat transfer rates for a 30° semi-apex angle blunt body flying at Mach 5.75

    Effect of coolant gas injection in the stagnation region on the surface heat transfer rates and aerodynamic drag for a large angle blunt body flying at hypersonic Mach number is reported for two stagnation ent...

    N. Sahoo, V. Kulkarni, G. Jagadeesh, K. P. J. Reddy in Shock Waves (2005)