All Stories

  1. Velocity and Temperature Measurements in High-speed Flows with Naturally Present Dust Particles Using Rayleigh and Mie Scattering

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

    Dr Jayanta Panda

  2. Verification of Calculation Procedure for Unsteady Aerodynamic Forces on a Launch Vehicle

    Article • Journal of Spacecraft and Rockets, November 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Jayanta Panda

  3. Verification of Calculation Procedure for Unsteady Aerodynamic Forces on a Launch Vehicle

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

    Dr Jayanta Panda

  4. Wavenumber-Frequency Spectra on a Launch Vehicle Model Measured via Unsteady Pressure-Sensitive Paint

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

    Dr Jayanta Panda, Jim Ross

  5. Verification of Calculation Procedure for Unsteady Aerodynamic Forces on a Launch Vehicle

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

    Dr Jayanta Panda

  6. A Spectrally-resolved Rayleigh scattering set-up to measure velocity and temperature in high-speed flows

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

    Dr Jayanta Panda

  7. Unsteady pressure fluctuations measured on a hammerhead space vehicle and comparison with Coe and Nute's 1962 data

    Article • International Journal of Aeroacoustics, February 2018, SAGE Publications

    Dr Jayanta Panda

  8. Spectral Analysis of the Acoustic Near Field of a Solid-Propellant Rocket

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

    Dr Jayanta Panda

  9. Experimental Verification of Buffet Calculation Procedure Using Unsteady Pressure-Sensitive Paint

    Article • Journal of Aircraft, September 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Jayanta Panda

  10. Spectral analysis of the acoustic near field of a solid propellant rocket

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

    Dr Jayanta Panda

  11. Wavenumber-Frequency Spectra of Pressure Fluctuations on a Generic Space Vehicle Measured via Fast-Response Pressure-Sensitive Paint

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

    Dr Jayanta Panda, Jim Ross

  12. Experimental Visualizations of a Generic Launch Vehicle Flow Field: Time-Resolved Shadowgraph and Infrared Imaging

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

    Jim Ross, Dr Jayanta Panda

  13. Wavenumber-Frequency Spectra of Pressure Fluctuations Measured via Fast Response Pressure Sensitive Paint

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

    Dr Jayanta Panda, Jim Ross

  14. A tool to measure fluctuations in density/temp in wind tunnels

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

    Dr Jayanta Panda

  15. Noise Source Identification During Rocket Engine Test Firings and a Rocket Launch

    Article • Journal of Spacecraft and Rockets, November 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Jayanta Panda

  16. Molecular Rayleigh scattering to measure fluctuations in density and temperature in low speed heated wind tunnel flows

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

    Dr Jayanta Panda