All Stories

  1. Impact of tab location relative to the nozzle exit on the shock structure of a supersonic jet

    Article • Physics of Fluids, July 2019, American Institute of Physics

    Professor Ethirajan Rathakrishnan, Manideep Aileni, Dr. Arun Kumar Perumal

  2. Empirical scaling analysis of supersonic jet control using steady fluidic injection

    Article • Physics of Fluids, May 2019, American Institute of Physics

    Professor Ethirajan Rathakrishnan, Dr. Arun Kumar Perumal

  3. Fluidic injectors for supersonic jet control

    Article • Physics of Fluids, December 2018, American Institute of Physics

    Professor Ethirajan Rathakrishnan, Dr. Arun Kumar Perumal

  4. Parametric study and scaling of jet manipulation using an unsteady minijet

    Article • Journal of Fluid Mechanics, June 2018, Cambridge University Press

    Dr. Arun Kumar Perumal

  5. Experimental Study of Subsonic and Sonic Jets Controlled by Air Tabs

    Article • Journal of Propulsion and Power, September 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Ethirajan Rathakrishnan, Dr. Arun Kumar Perumal

  6. Corrugated right-angled triangular tabs for supersonic jet control

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, December 2014, SAGE Publications

    Dr. Arun Kumar Perumal

  7. Triangular tabs for supersonic jet mixing enhancement

    Article • The Aeronautical Journal, November 2014, Cambridge University Press

    Dr. Arun Kumar Perumal