All Stories

  1. Effects of Various Geometric and Kinematic Parameters on the Cyclonic Flow Evolution in a Vortex Chamber

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Gaurav Sharma, Joseph Majdalani

  2. Effects of various geometric parameters on the computed swirl numbers and flow topology in a bidirectional vortex chamber

    Article • Physics of Fluids, January 2024, American Institute of Physics

    Dr. Gaurav Sharma

  3. Effects of Varying Characteristic Injection Parameters and Geometric Configurations on the Cyclonic Flowfield in a Bidirectional Vortex Chamber Using Velocity Inlet Conditions

    Article • January 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Gaurav Sharma

  4. Effects of Nozzle Inlet Size and Curvature on the Cyclonic Flowfield in a Bidirectional Vortex Chamber Using Velocity Inlet Conditions

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Gaurav Sharma, Joseph Majdalani

  5. Effects of various inlet parameters on the computed flow development in a bidirectional vortex chamber

    Article • Physics of Fluids, April 2022, American Institute of Physics

    Dr. Gaurav Sharma, Joseph Majdalani

  6. Effects of nozzle inlet size and curvature on the flow development in a bidirectional vortex chamber

    Article • Physics of Fluids, September 2021, American Institute of Physics

    Dr. Gaurav Sharma

  7. Effect of Variable Outlets on the Nonreactive Flowfield of a Right-Cylindrical Cyclonic Chamber

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Gaurav Sharma, Joseph Majdalani

  8. Characterization of the Cyclonic Flowfield in a Swirl Driven Combustion Chamber

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

    Dr. Gaurav Sharma

  9. Computational Fluid Dynamic Simulation of Single and Two-Phase Vortex Flow—A Comparison of Flow Field and Energy Separation

    Article • Journal of Heat Transfer, May 2016, ASME International

    Dr. Gaurav Sharma

  10. Numerical analysis of flow field over compound delta wing at subsonic and supersonic speeds

    Article • March 2016, Institute of Electrical & Electronics Engineers (IEEE)

    Dr. Gaurav Sharma

  11. Computational and experimental study of deflected nose of missile at subsonic speed

    Article • March 2015, Institute of Electrical & Electronics Engineers (IEEE)

    Dr. Gaurav Sharma