All Stories

  1. Heat Transport Processes of Film Cooling in Rocket Combustion Chambers

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

    Dmitry Suslov, Prof. Dr. Michael Oschwald, Georg Kühlwein

  2. Component Test Results and Project Progress of the DLR Liquid Upper Stage Demonstrator Engine (LUMEN)

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

    Michael Börner, Kai Dresia, Dmitry Suslov, Prof. Dr. Michael Oschwald

  3. Heat Transfer Prediction for Methane in Regenerative Cooling Channels with Neural Networks

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

    Prof. Dr. Michael Oschwald, Kai Dresia, Günther Waxenegger-Wilfing

  4. Active Control of Dual-Bell Nozzle Operation Mode Transition by Film Cooling and Mixture Ratio Variation

    Article • Journal of Propulsion and Power, January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Dr. Michael Oschwald

  5. Propellant Atomization for Porous Injectors

    Article • Journal of Propulsion and Power, November 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Dr. Michael Oschwald, Dmitry Suslov

  6. Experimental Study of Methane Heat Transfer Deterioration in a Subscale Combustion Chamber

    Article • Journal of Propulsion and Power, July 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Dr. Michael Oschwald, Dmitry Suslov

  7. Injector-Driven Flame Dynamics in a High-Pressure Multi-Element Oxygen–Hydrogen Rocket Thrust Chamber

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

    Prof. Dr. Michael Oschwald, Dmitry Suslov

  8. Numerical Model for Nozzle Flow Application Under Liquid Oxygen/Methane Hot-Flow Conditions

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

    Prof. Dr. Michael Oschwald, Sebastian Karl

  9. Comparison Between Excited Hydroxyl Radical and Blue Radiation from Hydrogen Rocket Combustion

    Article • Journal of Propulsion and Power, March 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Dr. Michael Oschwald, Dr. Thomas F. Sattelmayer, Dr. Robert Gerald Stützer

  10. Review of experimental test cases for modelling high frequency combustion instability (Invited paper)

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

    Prof. Dr. Michael Oschwald, Dmitry Suslov

  11. Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor

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

    Prof. Dr. Michael Oschwald, Dmitry Suslov

  12. Thermoacoustic Feedback Analysis of a Cylindrical Combustion Chamber under Supercritical Conditions

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

    Prof. Dr. Michael Oschwald, Dr. Thomas F. Sattelmayer

  13. Coupling of Cryogenic Oxygen–Hydrogen Flames to Longitudinal and Transverse Acoustic Instabilities

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

    Prof. Dr. Michael Oschwald