All Stories

  1. Control of Shock-Induced Flow Separation Using Rectangular Air-Jet Vortex Generators

    Article • Journal of Propulsion and Power, December 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.-Ing. Anne-Marie Schreyer

  2. Research configuration to study shock oscillation mechanisms in highly loaded transonic fans

    Article • Aerospace Science and Technology, November 2025, Elsevier

    Dr.-Ing. Anne-Marie Schreyer

  3. Influences in Experimental Studies on the Characteristics of Transonic Shock Buffet

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

    Dr.-Ing. Anne-Marie Schreyer

  4. On the Wake/Tailplane Interaction for Established Transonic Airfoil Buffet

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

    Dr.-Ing. Anne-Marie Schreyer

  5. Shock Oscillation Mechanisms of Highly Separated Transitional Shock-Wave/Boundary-Layer Interactions

    Article • January 2025, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  6. Shock Oscillation Mechanism of Highly Separated Transitional Shock-Wave/Boundary-Layer Interactions

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

    Philipp Leonard Nel, Dr.-Ing. Anne-Marie Schreyer

  7. Analysis of a transitional shock-wave/boundary-layer interaction with strong separation

    Article • Physics of Fluids, November 2024, American Institute of Physics

    Philipp Leonard Nel, Dr.-Ing. Anne-Marie Schreyer

  8. Effect of Transition on Self-Sustained Shock Oscillations in Highly Loaded Transonic Rotors

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

    Dr.-Ing. Anne-Marie Schreyer

  9. Design considerations for efficient spanwise-inclined air-jet vortex generators for separation control in supersonic and hypersonic flows

    Article • Aerospace Science and Technology, April 2024, Elsevier

    Dr.-Ing. Anne-Marie Schreyer

  10. Flow fields around asymmetrical micro vortex generators in supersonic flow

    Article • Aerospace Science and Technology, February 2024, Elsevier

    Dr.-Ing. Anne-Marie Schreyer

  11. 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

  12. Effects of jet-injection-pipe length on the flow-control effectiveness of spanwise-inclined jets in supersonic crossflow

    Article • Physical Review Fluids, November 2023, American Physical Society (APS)

    Dr.-Ing. Anne-Marie Schreyer

  13. Control of shock-induced separation using air-jet vortex generators

    Article • November 2023, Cassyni

    Dr.-Ing. Anne-Marie Schreyer

  14. Forced Injection of a Spanwise-Inclined Jet in Supersonic Crossflow

    Article • AIAA Journal, September 2023, American Institute of Aeronautics and Astronautics (AIAA)

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

  15. Effects of Jet-Orifice Shape on the Flow-Control Effectiveness of Air-Jet Vortex Generators

    Article • September 2023, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  16. Effects of favourable downstream pressure gradients on separated shock-wave/boundary-layer interactions

    Article • International Journal of Heat and Fluid Flow, August 2023, Elsevier

    Dr.-Ing. Anne-Marie Schreyer

  17. Experimental Analysis of Transonic Buffet Conditions on a Two-Dimensional Supercritical Airfoil

    Article • AIAA Journal, August 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.-Ing. Anne-Marie Schreyer

  18. Numerical analysis of the flow around a speed skydiver

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

    Dr.-Ing. Anne-Marie Schreyer

  19. Spanwise-Inclined Jets in Supersonic Crossflow: Effects of Injection Pressure and Separation-Control Effectiveness

    Article • AIAA Journal, June 2023, American Institute of Aeronautics and Astronautics (AIAA)

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

  20. Separation control with elliptical air-jet vortex generators

    Article • Experiments in Fluids, May 2023, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer

  21. 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

  22. 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

  23. 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

  24. 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

  25. 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

  26. 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

  27. 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

  28. 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

  29. 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

  30. 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

  31. 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

  32. 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

  33. 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

  34. 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

  35. 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

  36. 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

  37. 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

  38. 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

  39. Velocity Spectrum Estimation in Shock-Boundary Layer Interaction

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

    Dr.-Ing. Anne-Marie Schreyer

  40. 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

  41. 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

  42. 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

  43. 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

  44. 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

  45. 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

  46. 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

  47. 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

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

    Article • November 2009, Springer Science + Business Media

    Dr.-Ing. Anne-Marie Schreyer