All Stories

  1. Effect of Low and High-Fidelity Thermochemical Models on Hypersonic Nonequilibrium Flows

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

    Eswar Josyula

  2. Multiquantum Transitions in Oxygen and Nitrogen Molecules in Hypersonic Nonequilibrium Flows

    Article • Journal of Thermophysics and Heat Transfer, November 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  3. Wall Boundary Conditions in Hypersonic Thermochemical Nonequilibrium Flows

    Article • June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  4. Direct Simulation Monte Carlo Modeling of Gas Electronic Excitation for Hypersonic Sensing

    Article • Journal of Thermophysics and Heat Transfer, October 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  5. Vibrational Nonequilibrium Quantification for State-Resolved Simulation of a Hypersonic Flow

    Article • Journal of Thermophysics and Heat Transfer, July 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  6. State-to-State Kinetic Modeling of Select Air Species in Hypersonic Nonequilibrium Flows

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

    Eswar Josyula

  7. Double-Cone Flows in Nonequilibrium: Comparison of CFD with Experimental Data

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

    Eswar Josyula

  8. Role of High Fidelity Nonequilibrium Modeling in Laminar and Turbulent Flows for High Speed ISR Missions

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  9. State-to-State Kinetic Modeling of Oxygen in Hypersonic Nonequilibrium Flows

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  10. Adaptive State Resolved Vibrational Energy Modeling for Hypersonic Flow Simulation

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  11. Non-equilibrium hypersonic flow

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  12. Assessment of Vibrational Nonequilibrium for State Resolved Simulation of a Hypersonic Flow

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  13. Computational Study of Non-Equilibrium Effects on Hypersonic Boundary-Layer Transition

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  14. Global Sensitivity Analysis and Uncertainty Quantification for a Hypersonic Shock Interaction Flow

    Article • Journal of Thermophysics and Heat Transfer, July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  15. DSMC Modeling of Nonequilibrium Electronic Excitation and Emission for Hypersonic Sensor Applications

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  16. State-to-State Kinetic Model for a Viscous Radiating Hypersonic Flow

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula, Prof Elena Kustova

  17. Nonequilibrium Radiation Modeling for a Low Enthalpy Hypersonic Shock Layer

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  18. Uncertainty Quantification for a Scramjet Inlet Flow

    Article • July 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  19. A Direct Simulation Monte Carlo Collision Limiter Scheme for Efficient Simulation of Viscous Continuum Flows

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  20. Efficient Direct Simulation Monte Carlo Modeling of Very Low Knudsen Number Gas Flows

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula

  21. Influence of State-to-State Transport Coefficients on Surface Heat Transfer in Hypersonic Flows

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Eswar Josyula, Prof Elena Kustova