All Stories

  1. Modification of Eigenmodes in a Cold-Flow Rocket Combustion Chamber by Acoustic Resonators

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

    Dr. Thomas F. Sattelmayer

  2. Numerical Investigation of Reacting Flow in a Methane Rocket Combustor: Turbulence Modeling

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

    Dr. Thomas F. Sattelmayer

  3. Combustion Noise Prediction Using Linearized Navier–Stokes Equations and Large-Eddy Simulation Sources

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

    Dr. Thomas F. Sattelmayer

  4. 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

  5. Numerical Modeling of Flow and Combustion in a Single-Element GCH4/GOX Rocket Combustor: Aspects of Turbulence Modeling

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

    Dr. Thomas F. Sattelmayer

  6. Numerical Investigation of Flow and Combustion in a Single-Element GCH4/GOX Rocket Combustor: Chemistry Modeling and Turbulence-Combustion Interaction

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

    Dr. Thomas F. Sattelmayer, Dr Laurent Selle

  7. Numerical Investigation of Flow and Combustion in a Single Element GCH4/Gox Rocket Combustor

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

    Dr. Thomas F. Sattelmayer, Dr Laurent Selle

  8. Computation of Combustion Noise from a Premixed and Pressurized Propane Flame Using Statistical Noise Modeling

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

    Dr. Thomas F. Sattelmayer

  9. Measurement and Analysis of Flame Transfer Functions in a Lean-Premixed, Swirl-Stabilized Combustor with Water Injection

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

    Dr. Thomas F. Sattelmayer

  10. Flamelet Generated Manifolds for Partially Premixed, Highly Stretched and Non-Adiabatic Combustion in Gas Turbines

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

    Dr. Thomas F. Sattelmayer

  11. Radiation-Based Validation of Combustion Simulations and Comparison to Heat Release in Rocket Engines

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

    Dr. Thomas F. Sattelmayer

  12. Impact of Injector Mass Flow Fluctuations on Combustion Dynamics in Liquid Engines

    Article • Journal of Spacecraft and Rockets, September 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Thomas F. Sattelmayer

  13. Interaction of Combustion with Transverse Velocity Fluctuations in Liquid Rocket Engines

    Article • Journal of Propulsion and Power, July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Thomas F. Sattelmayer

  14. Validation of Transverse Instability Damping Computations for Rocket Engines

    Article • Journal of Propulsion and Power, July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Thomas F. Sattelmayer

  15. Numerical Investigation of Indirect Noise Generation by Accelerated Vorticity

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

    Dr. Thomas F. Sattelmayer

  16. Acoustic Scattering Matrices for Higher-Order Modes for Simple Orifice Configurations with Flow

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

    Dr. Thomas F. Sattelmayer

  17. Transfer Functions of Acoustic, Entropy and Vorticity Waves in an Annular Model Combustor and Nozzle for the Prediction of the Ratio Between Indirect and Direct Combustion Noise

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

    Dr. Thomas F. Sattelmayer

  18. Impact of Absorber Ring Position and Cavity Length on Acoustic Damping

    Article • Journal of Spacecraft and Rockets, May 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Thomas F. Sattelmayer

  19. Eigenvalue Analysis for the Prediction of Initial Growth Rates of Thermoacoustic Instability in Rocket Motors

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

    Dr. Thomas F. Sattelmayer

  20. 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

  21. Low-Order Modelling of the Non-Local Acoustic Reacting Combustion Chamber-Dome Interface in Rocket Engines

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

    Dr. Thomas F. Sattelmayer

  22. Semi-Zonal Hybrid RANS/LES Turbulence Modeling with RANS Sensor Based Interfacing Applied to Supersonic Flows

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

    Dr. Thomas F. Sattelmayer

  23. Validation of a Novel OpenFOAM Solver using a Supersonic, Non-reacting Channel Flow

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

    Paul Nizenkov, Dr. Thomas F. Sattelmayer

  24. Acoustic-entropy coupling behavior and acoustic scattering properties of a Laval nozzle

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

    Dr. Thomas F. Sattelmayer

  25. Unsteady RANS Investigation of a Hydrogen-Fueled Staged Supersonic Combustor with Lobed Injectors

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

    Dr. Thomas F. Sattelmayer

  26. Determination of Acoustic Scattering Matrices Using Nonlinear Disturbance Equations

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

    Dr. Thomas F. Sattelmayer