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    Article

    Study of unsteadiness due to 3-D shock–boundary layer interaction in flow over a square-faced protuberance

    The dynamics of shock-induced unsteady separated flow past a three-dimensional square-faced protuberance are investigated through wind tunnel experiments. Time-resolved schlieren imaging and unsteady surface p...

    K. Ramachandra, S. Bhardwaj, J. N. Murugan, R. Sriram in Shock Waves (2023)

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    Chapter and Conference Paper

    Solar Energy Simulation of Fresnel Lens Concentrated System for Thermal Electric Generator

    The expensive manufacturing process and low efficiency at high working temperature of Solar cells necessitate the need for an alternate solar energy generation system. Solar concentrated thermal electric syste...

    S. Babu, R. Sriram, S. Gopikrishnan, A. Praveen in Fluid Mechanics and Fluid Power (2021)

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    Chapter and Conference Paper

    Flow Visualization and Computational Studies on Unsteadiness Due to 3-D Shock-Induced Separation of Flow Over a Square Protrusion

    Strong shock interaction with the boundary layer in high speed flows results in boundary layer separation. They are associated with low frequency oscillations of the separation shock whose origin has been a so...

    K. Ramachandra, S. Bhardwaj, R. Sriram in Fluid Mechanics and Fluid Power (2021)

  4. Article

    Open Access

    Experimental investigations on the sharp leading-edge separation over a flat plate at zero incidence using particle image velocimetry

    Leading-edge separated flow field over a sharp flat plate is experimentally investigated in Reynolds numbers ranging from 6.2 × 103 to 4.1 × 104, using particle image velocimetry (PIV) and its statistics. It was ...

    K. Fujiwara, R. Sriram, K. Kontis in Experiments in Fluids (2020)

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    Chapter and Conference Paper

    Reynolds Number Effects on Shock Wave Boundary Layer Interaction in a Hypersonic Flow

    The Reynolds number is found to affect the separation bubble for shock im**ement locations away from the leading edge where finite separation occurs. A decrease in separation bubble was observed with an incr...

    L. Srinath, S. Mohammed Ibrahim, R. Sriram in 31st International Symposium on Shock Wave… (2019)

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    Chapter and Conference Paper

    Review on Film Cooling in High-Speed Flows

    This review presents the state of the art in film cooling applied to high-speed flows. Film cooling is a promising technique to reduce heat transfer and shield a surface that is exposed to high-temperature cor...

    K. Fujiwara, R. Sriram, K. Kontis in 31st International Symposium on Shock Waves 2 (2019)

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    Chapter and Conference Paper

    Effectiveness of Film Cooling over Large Angle Blunt Cones in High Speed Carbon Dioxide Flows

    In the last four decades more than a dozen of spacecrafts have been sent to planet Mars for its exploration[1].

    S. Mohammed Ibrahim, R. Sriram in 29th International Symposium on Shock Wav… (2015)

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    Chapter and Conference Paper

    Shock Tunnel Investigations on Im**ing Shock Wave Boundary Layer Interactions at Hypersonic Speeds

    The interaction between shock wave and boundary layer continues to be interesting area of research for over six decades. Extensive research works have illuminated various aspects of the interaction, especially...

    R. Sriram, Mohammed Ibrahim, G. Jagadeesh in 29th International Symposium on Shock Wav… (2015)

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    Chapter and Conference Paper

    Experimental Investigations on the Effect of Dielectric Barrier Discharge on the Hypersonic Flow Around a Flat Plate

    Surface dielectric barrier discharges (DBD) are known to offer potential flow control techniques for low speed flows. A well known application of DBD in low speed flows is separation control as illustrated by ...

    R. Sriram, G. Jagadeesh, K. P. J. Reddy in 28th International Symposium on Shock Waves (2012)

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    Chapter and Conference Paper

    Density Field Measurements of a Micro–explosion Using BOS

    The flow field dynamics associated with blast waves can be better understood by generating controlled micro-explosions in the laboratory. In recent years microexplosions have also found interesting trans-disci...

    P. Suriyanarayanan, N. Karthikeyan in 28th International Symposium on Shock Waves (2012)

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    Chapter and Conference Paper

    Effect of Dielectric Barrier Discharge Plasma in Supersonic Flow

    In the recent past, there is a growing interest in using the Dielectric Barrier Discharge (DBD) based plasma actuators for active control of the boundary layer in different speed regimes. The plasma actuators ...

    Suparna Pal, R. Sriram, M. V. Srisha Rao in 28th International Symposium on Shock Waves (2012)