All Stories

  1. Validation of Ablation Model of PICA Using Fully Implicit Ablation and Thermal Response Program

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

    Dr Mark - Salita, Joseph Koo

  2. Model of Plume Flowfield from Oxy-Acetylene Torch

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

    Dr Mark - Salita, Joseph Koo

  3. Unanticipated Problems and Misunderstood Phenomena in and Around Solid Rockets

    Article • July 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  4. Modern SRM ignition transient modeling. I - Introduction and physical models

    Article • July 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  5. Evaluation of CFD code CFD-ACE for application to rocket problems

    Article • July 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  6. Closed-form analytical solutions for fluid mechanical, thermochemical, and thermal processes in solid rocket motors

    Article • July 1998, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  7. Modeling of ignition overpressure in Minuteman silos

    Article • July 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  8. Predicted slag deposition histories in eight solid rocket motors using the CFD model 'EVT'

    Article • July 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  9. Deficiencies and requirements in modeling of slag generation in solid rocket motors

    Article • Journal of Propulsion and Power, January 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  10. VORSTREM - A simple and versatile 2D viscous solver for chamber flow in solid rocket motors

    Article • June 1994, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  11. Use of water and mercury droplets to simulate Al2O3 collision/coalescence in rocket motors

    Article • Journal of Propulsion and Power, July 1991, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  12. Comparison of four boundary layer solutions for fuel regression ratein classical hybrid rocket motors

    Article • June 1991, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  13. Verification of spatial and temporal pressure distributions in segmented solid rocket motors

    Article • January 1989, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  14. Simple finite-element model of O-ring deformation and activation during squeeze and pressurization

    Article • Journal of Propulsion and Power, November 1988, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita

  15. A simple finite-element model of O-ring deformation and activation during squeeze and pressurization

    Article • June 1987, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mark - Salita