All Stories

  1. Computational Analysis of Two Mars Powered Descent Vehicle Concepts Tested in the Langley Unitary Plan Wind Tunnel

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

    Francisco Canabal, Heather Houlden

  2. Base Heating Environment During Ground Testing of a Lunar Lander Demonstrator

    Article • Journal of Thermophysics and Heat Transfer, October 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  3. Hydrogen Containment Process for Nuclear Thermal Engine Ground Testing

    Article • Journal of Propulsion and Power, January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  4. Three-Dimensional Analysis of a Hydrogen Containment Process For Nuclear Thermal Engine Ground Testing

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

    Francisco Canabal

  5. Numerical Base Heating Sensitivity Study for a Four-Rocket Engine Core Configuration

    Article • Journal of Spacecraft and Rockets, May 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  6. Thermal Hydraulics Design and Analysis Methodology for a Solid-Core Nuclear Thermal Rocket Engine Thrust Chamber

    Article • February 2013, IntechOpen

    Francisco Canabal

  7. Multiphysics Computational Analysis of a Solid-Core Nuclear Thermal Engine Thrust Chamber

    Article • Journal of Propulsion and Power, May 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  8. Multiphysics Computational Analysis of a Solid-Core Nuclear Thermal Engine Thrust Chamber

    Article • June 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  9. Study of the Ignition Overpressure Suppression Technique by Water Addition

    Article • Journal of Spacecraft and Rockets, July 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  10. Multiphysics Analysis of a Solid-Core Nuclear Thermal Engine Thrust Chamber

    Article • June 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  11. Control of Combustion-Instabilities Through Various Passive Devices

    Article • May 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  12. Suppression of Ignition Overpressure Generated by Launch Vehicles

    Article • May 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  13. On the Suppression of Ignition Overpressure Generated by Launch Vehicles

    Article • May 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  14. A Finite Element Based Flux Correction Scheme for the Euler Equations

    Article • May 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  15. A Computational Study of Ignition Over-Pressure for Launch Vehicles

    Article • June 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal

  16. Unified CFD methods via flowfield-dependent variation theory

    Article • June 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal