All Stories

  1. Shock-Boundary Layer Interaction Control using Innovative Micro-Vortex Generators in Supersonic Intake

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Mrinal Kaushik, Miss Humrutha G, Professor K P Sinhamahapatra

  2. Shock Boundary Layer Interaction Control in Supersonic Intake using Cavity with Porous Surface

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Mrinal Kaushik, Miss Humrutha G, Professor K P Sinhamahapatra

  3. Tab Aspect Ratio Effect on Supersonic Jet Mixing

    Article • International Journal of Turbo and Jet Engines, January 2015, De Gruyter

    Professor Ethirajan Rathakrishnan, Mrinal Kaushik