All Stories

  1. Enabling Resolvent Analysis Through Assimilation of Experimental Mean Flows with Physics-Informed Neural Networks: A Case Study on the Boeing Gaussian Bump

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Moritz Reumschüssel, Dr Kilian Oberleithner

  2. Wavepackets Driving Trailing Edge Noise. Part II – Resolvent-Based Model

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

    Dr. André V. G. Cavalieri, Ardeshir Hanifi, Dr Kilian Oberleithner

  3. Wavepackets Driving Trailing Edge Noise. Part I – Direct Simulation and Experiments

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

    Dr Kilian Oberleithner, Dr. André V. G. Cavalieri, Ardeshir Hanifi

  4. Uncertainty Quantification of Kiel Probes for RDC Applications

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Mohammad Rezay Haghdoost, Dr Kilian Oberleithner

  5. Predicting Wind Turbine Wake Breakdown Using a Free Vortex Wake Code

    Article • AIAA Journal, November 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Kilian Oberleithner

  6. High-Speed Schlieren and Particle Image Velocimetry of the Exhaust Flow of a Pulse Detonation Combustor

    Article • AIAA Journal, August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Kilian Oberleithner, Mohammad Rezay Haghdoost

  7. Predicting Wind Turbine Wake Breakdown Using a Free Vortex Wake Code

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

    Dr Kilian Oberleithner

  8. Investigation of the Exhaust Flow of a Pulse Detonation Combustor at different Operating Conditions based on High-Speed Schlieren and PIV

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

    Dr Kilian Oberleithner, Mohammad Rezay Haghdoost

  9. Shear flow instabilities in swirl-stabilized combustors and their impact on the amplitude dependent flame response: A linear stability analysis

    Article • Combustion and Flame, January 2015, Elsevier

    Dr Kilian Oberleithner

  10. Vortex Breakdown Types and Global Modes in Swirling Combustor Flows with Axial Injection

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

    Dr Kilian Oberleithner

  11. Mean flow stability analysis of oscillating jet experiments

    Article • Journal of Fluid Mechanics, September 2014, Cambridge University Press

    Dr Kilian Oberleithner

  12. Impact of Steam-Dilution on the Flame Shape and Coherent Structures in Swirl-Stabilized Combustors

    Article • Combustion Science and Technology, May 2014, Taylor & Francis

    Dr Kilian Oberleithner

  13. Coherent structure and sound production in the helical mode of a screeching axisymmetric jet

    Article • Journal of Fluid Mechanics, May 2014, Cambridge University Press

    Dr Kilian Oberleithner

  14. Impact of Shear Flow Instabilities on the Magnitude and Saturation of the Flame Response

    Article • Journal of Engineering for Gas Turbines and Power, February 2014, ASME International

    Dr Kilian Oberleithner

  15. On the impact of swirl on the growth of coherent structures

    Article • Journal of Fluid Mechanics, February 2014, Cambridge University Press

    Dr Kilian Oberleithner

  16. Application of linear hydrodynamic stability analysis to reacting swirling combustor flows

    Article • Journal of Fluid Science and Technology, January 2014, Japan Society of Mechanical Engineers

    Dr Kilian Oberleithner

  17. Why Nonuniform Density Suppresses the Precessing Vortex Core

    Article • Journal of Engineering for Gas Turbines and Power, September 2013, ASME International

    Dr Kilian Oberleithner

  18. Vortex Breakdown and Global Modes in Swirling Combustor Flows with Axial Air Injection

    Article • June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Kilian Oberleithner

  19. Why Non-Uniform Density Suppresses the Precessing Vortex Core

    Article • June 2013, ASME International

    Dr Kilian Oberleithner

  20. Impact of Shear Flow Instabilities on the Magnitude and Saturation of the Flame Response

    Article • June 2013, ASME International

    Dr Kilian Oberleithner

  21. Formation of Turbulent Vortex Breakdown: Intermittency, Criticality, and Global Instability

    Article • AIAA Journal, July 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Kilian Oberleithner

  22. On the Impact of Shear Flow Instabilities on Global Heat Release Rate Fluctuations: Linear Stability Analysis of an Isothermal and a Reacting Swirling Jet

    Article • June 2012, ASME International

    Dr Kilian Oberleithner

  23. Salt overload damages the glycocalyx sodium barrier of vascular endothelium

    Article • Pflügers Archiv - European Journal of Physiology, July 2011, Springer Science + Business Media

    Dr Kilian Oberleithner

  24. Low Amplitude Excitation of Moderately Swirling Jets at High Reynolds Numbers

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Kilian Oberleithner