All Stories

  1. On the Wake/Tailplane Interaction in Established Transonic Shock Buffet Mode

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

    Dr.-Ing. Anne-Marie Schreyer

  2. Numerical analysis of the flow around a speed skydiver

    Article • European Journal of Mechanics - B/Fluids, July 2023, Elsevier

    Dr.-Ing. Anne-Marie Schreyer

  3. Influence of jet spacing in spanwise-inclined jet injection in supersonic crossflow

    Article • Journal of Fluid Mechanics, August 2022, Cambridge University Press

    Dr.-Ing. Anne-Marie Schreyer

  4. Flow fields around spanwise-inclined elliptical jets in supersonic crossflow

    Article • European Journal of Mechanics - B/Fluids, July 2022, Elsevier

    Dr.-Ing. Anne-Marie Schreyer

  5. Spanwise-inclined Injection of Unsteady Jets in Supersonic Crossflow

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Robin Sebastian, Dr.-Ing. Anne-Marie Schreyer

  6. Effects of Jet-to-Jet Spacing of Air-Jet Vortex Generators in Shock-Induced Flow-Separation Control

    Article • Flow Turbulence and Combustion, April 2022, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  7. Influence of a Microramp Array on a Hypersonic Shock-Wave/Turbulent Boundary-Layer Interaction

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

    Dr.-Ing. Anne-Marie Schreyer

  8. Control of Shock-Induced Separation of a Turbulent Boundary Layer Using Air-Jet Vortex Generators

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

    Dr.-Ing. Anne-Marie Schreyer

  9. Dynamics and Unsteady Features of the Turbulent Separation over a Forward-Facing Step

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

    Dr.-Ing. Anne-Marie Schreyer

  10. Flow field around a spanwise-inclined jet in supersonic crossflow

    Article • Aerospace Science and Technology, September 2020, Elsevier

    Dr.-Ing. Anne-Marie Schreyer, Dr. Robin Sebastian

  11. Flow structure in the wake of a space-launcher model with propulsive-jet simulation

    Article • CEAS Space Journal, March 2020, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  12. Influence of Jet Spacing and Injection Pressure on Separation Control with Air-Jet Vortex Generators

    Article • September 2019, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  13. Effect of Jet Spacing in Separation Control with Air Jet Vortex Generators

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

    Dr.-Ing. Anne-Marie Schreyer

  14. Experimental Investigation of Two Hypersonic Shock/Turbulent Boundary-Layer Interactions

    Article • AIAA Journal, December 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.-Ing. Anne-Marie Schreyer, Professor Alexander J Smits, Dr. Owen J Williams

  15. Separation Control with Lobe Mixers in the Wake of an Axisymmetric Space-Launcher Model

    Article • October 2017, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  16. Velocity Spectrum Estimation in Shock-Wave/Turbulent Boundary-Layer Interaction

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

    Dr.-Ing. Anne-Marie Schreyer

  17. Characterization of the supersonic wake of a generic space launcher

    Article • CEAS Space Journal, July 2016, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  18. Characterization of an incipiently separated shock wave/turbulent boundary layer interaction

    Article • Shock Waves, May 2016, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  19. Analysis of acoustic and entropy disturbances in a hypersonic wind tunnel

    Article • Physics of Fluids, May 2016, American Institute of Physics

    Dr.-Ing. Anne-Marie Schreyer

  20. Method for Spectra Estimation from High-Speed Experimental Data

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

    Dr.-Ing. Anne-Marie Schreyer

  21. Velocity Spectrum Estimation in Shock-Boundary Layer Interaction

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

    Dr.-Ing. Anne-Marie Schreyer

  22. Flow structure and unsteadiness in the supersonic wake of a generic space launcher

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

    Dr.-Ing. Anne-Marie Schreyer

  23. Development of a Dual-PIV system for high-speed flow applications

    Article • Experiments in Fluids, September 2015, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  24. Particle response analysis for particle image velocimetry in supersonic flows

    Article • Physics of Fluids, July 2015, American Institute of Physics

    Dr.-Ing. Anne-Marie Schreyer, Dr. Owen J Williams

  25. Method for spectra estimation from high-speed experimental data at discrete points in time

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

    Dr.-Ing. Anne-Marie Schreyer

  26. Experiments on the Influence of a Microramp Array on a Hypersonic Shock Turbulent Boundary Layer Interaction

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

    Professor Alexander J Smits, Dr.-Ing. Anne-Marie Schreyer

  27. Turbulence Measurements with PIV in a Hypersonic Shock Boundary Layer Interaction

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

    Professor Alexander J Smits, Dr.-Ing. Anne-Marie Schreyer

  28. Experimental Investigations of a Hypersonic Shock Turbulent Boundary Layer Interaction

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

    Professor Alexander J Smits, Dr.-Ing. Anne-Marie Schreyer

  29. Experimental Flow Studies on Separation and Reattachment in the Vicinity of Sharp,Wedge Shaped Leading Edges at Low Reynolds Numbers

    Article • January 2010, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  30. Fluctuation Measurements in the Turbulent Boundary Layer of a Supersonic Flow

    Article • November 2009, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer