All Stories

  1. Computational Simulation of Axis Symmetric Aft Wall Angle Cavity in Supersonic Flow Field

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

    Dr. Jeyakumar SUPPANDIPILLAI, jayaraman kandasamy, Naresh Relangi

  2. Ultra‐Fine Aluminium Characterization and its Agglomeration Features in Solid Propellant Combustion for Various Quenched Distance and Pressure

    Article • Propellants Explosives Pyrotechnics, February 2020, Wiley

    jayaraman kandasamy

  3. Quench Collection and Artificial Neural Network Prediction of Micro and Ultra-fine Aluminum Agglomeration Phenomena in Combustion of Solid Rocket Propellants: Experiments and Modeling

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    V VENKATESWARA RAO, Tejasvi K, jayaraman kandasamy

  4. Sensitivity Analysis of Solid Propellant Burn Rate Measurements Using Ultrasound Technique by Different Data Deduction Methods

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Robin Rathi, AZIM HASHMI M, jayaraman kandasamy

  5. Effect of Axisymmetric Aft Wall Angle Cavity in Supersonic Flow Field

    Article • International Journal of Turbo and Jet Engines, February 2018, De Gruyter

    Dr. Jeyakumar SUPPANDIPILLAI, jayaraman kandasamy