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Publications

2026
POD Analysis of Shock / Turbulent Boundary Layer Interactions under Separation Control[DOI]
Ramaswamy, Deepak Prem; Schreyer, Anne-Marie
New results in numerical and experimental fluid mechanics XV : contributions to the 24th STAB/DGLR Symposium, Regensburg, Germany, 2024 / Andreas Dillmann, Gerd Heller, Ewald Krämer, Christian Breitsamter, Claus Wagner, Lars Krenkel 156 525-534 (2026)
Control of Shock-Induced Flow Separation Using Rectangular Air-Jet Vortex Generators[DOI]
Ramaswamy, Deepak Prem; Schreyer, Anne-Marie
Journal of propulsion and power 42-1 3-19 (2026)
2025
Characteristics of Shock Unsteadiness Towards Onset and Offset of Transonic Buffet[DOI]
Schauerte, Christopher Julian; Schreyer, Anne-Marie
[2025 AIAA Aviation Forum and Ascend, 2025-07-21 - 2025-07-25, Las Vegas, NV, USA] (2025)
On the Wake/Tailplane Interaction for Established Transonic Airfoil Buffet[DOI]
Schauerte, Christopher Julian; Schreyer, Anne-Marie
AIAA journal 63-7 2731-2749 (2025)
2024
Effects of Jet-Orifice Shape on the Flow-Control Effectiveness of Air-Jet Vortex Generators[DOI]
Ramaswamy, Deepak Prem; Schreyer, Anne-Marie
New results in numerical and experimental fluid mechanics XIV : contributions to the 23rd STAB/DGLR Symposium, Berlin, Germany, 2022 / Andreas Dillmann, Gerd Heller, Ewald Krämer, Claus Wagner, Julien Weiss editors 154 99-108 (2024)
Spatial And Temporal Modes On A Generic Tandem Configuration In Transonic Shock Buffet[DOI]
Schauerte, Christopher Julian; Schreyer, Anne-Marie
Proceedings of the 21st International Symposium on the Applications of Laser and Imaging Techniques to Fluid Mechanics : 8 - 11 July, 2024, Lisbon 19 Seiten (2024)
Flow fields around asymmetrical micro vortex generators in supersonic flow[DOI]
Hristozova, Lilia; Sebastian, Robin; Schreyer, Anne-Marie
Aerospace science and technology 145 108838 (2024)
On the Wake/Tailplane Interaction in Established Transonic Shock Buffet Mode[DOI]
Schauerte, Christopher Julian; Schreyer, Anne-Marie
AIAA SCITECH 2024 Forum : 8-12 January 2024, Orlando, FL AIAA 2024-1946 (2024)
Shock Oscillation Mechanism of Highly Separated Transitional Shock-Wave/Boundary-Layer Interactions[DOI]
Nel, Philipp L.; Schreyer, Anne-Marie; Schrijer, Ferry F. J.; van Oudheusden, Bas W.; Janke, Christian; Vasilopoulos, Ilias; Swoboda, Marius
AIAA journal 63-5 1703-1715 (2024)
Influences in Experimental Studies on the Characteristics of Transonic Shock Buffet[DOI]
Schauerte, Christopher Julian; Schreyer, Anne-Marie
AIAA journal 63-4 1209-1652 (2024)
Highly separated transitional shock-wave/boundary-layer interactions: A spatial modal study[DOI]
Nel, Philipp L.; Schreyer, Anne-Marie; Schrijer, Ferry F. J.; van Oudheusden, Bas W.; Swoboda, Marius
Physics of fluids 36-11 116114 (2024)
Effect of Transition on Self-Sustained Shock Oscillations in Highly Loaded Transonic Rotors[DOI]
Nel, Philipp L.; Janke, Christian; Vasilopoulos, Ilias; Swoboda, Marius; Schreyer, Anne-Marie; Hady, Ahmed; Flaszyński, Paweł
AIAA journal 62-6 2063-2075 (2024)
Design considerations for efficient spanwise-inclined air-jet vortex generators for separation control in supersonic and hypersonic flows[Open Access]
Sebastian, Robin; Schreyer, Anne-Marie
Aerospace science and technology 147 109033 (2024)
Experimental investigation on the turbulent wake flow in fully established transonic buffet conditions[Open Access]
Schauerte, Christopher Julian; Schreyer, Anne-Marie
CEAS Aeronautical Journal 15-1 125-147 (2024)
Forced Injection of a Spanwise-Inclined Jet in Supersonic Crossflow[DOI]
Sebastian, Robin; Schreyer, Anne-Marie
AIAA journal 62-1 52-64 (2024)
2023
Control of shock-induced flow separation with Air-Jet vortex generators[Open Access]
Ramaswamy, Deepak Prem
(Schreyer, Anne-Marie; Schröder, Wolfgang; Sandham, Neil)
PhD Thesis (2023)
Effects of jet-injection-pipe length on the flow-control effectiveness of spanwise-inclined jets in supersonic crossflow[DOI]
Ramaswamy, Deepak Prem; Sebastian, Robin; Schreyer, Anne-Marie
Physical review fluids 8-11 113902 (2023)
Numerical analysis of the flow around a speed skydiver[DOI]
Schölzel, Steffen; Henze, Andreas; Schreyer, Anne-Marie
European journal of mechanics / B 100 163-178 (2023)
Effects of favourable downstream pressure gradients on separated shock-wave/boundary-layer interactions[DOI]
LarchevĂŞque, Lionel; Ramaswamy, Deepak Prem; Schreyer, Anne-Marie
The international journal of heat and fluid flow 102 109164 (2023)
Spanwise-Inclined Jets in Supersonic Crossflow : Effects of Injection Pressure and Separation-Control Effectiveness[DOI]
Sebastian, Robin; Ramaswamy, Deepak Prem; Schreyer, Anne-Marie
AIAA journal 61-9 3833-3847 (2023)
Separation control with elliptical air-jet vortex generators[Open Access]
Ramaswamy, Deepak Prem; Schreyer, Anne-Marie
Experiments in fluids 64-5 105 (2023)
Experimental Analysis of Transonic Buffet Conditions on a Two-Dimensional Supercritical Airfoil[DOI]
Schauerte, Christopher Julian; Schreyer, Anne-Marie
AIAA journal 61-8 3432-3448 (2023)
2022
Influence of jet spacing in spanwise-inclined jet injection in supersonic crossflow[DOI]
Sebastian, Robin; Schreyer, Anne-Marie
Journal of fluid mechanics 946 A39 (2022)
Flow fields around spanwise-inclined elliptical jets in supersonic crossflow[DOI]
Sebastian, Robin; Schreyer, Anne-Marie
European journal of mechanics / B 94 299-313 (2022)
Effects of Jet-to-Jet Spacing of Air-Jet Vortex Generators in Shock-Induced Flow-Separation Control[Open Access]
Ramaswamy, Deepak Prem; Schreyer, Anne-Marie
Flow, turbulence and combustion 109-1 35-64 (2022)
2021
Influence of a Microramp Array on a Hypersonic Shock-Wave/Turbulent Boundary-Layer Interaction[DOI]
Schreyer, Anne-Marie; Sahoo, Dipankar; Williams, Owen J. H.; Smits, Alexander J.
AIAA journal 59-6 1924-1939 (2021)
Control of Shock-Induced Separation of a Turbulent Boundary Layer Using Air-Jet Vortex Generators[DOI]
Ramaswamy, Deepak Prem; Schreyer, Anne-Marie
AIAA journal 59-3 927-939 (2021)
2020
Influence of Jet Spacing and Injection Pressure on Separation Control with Air-Jet Vortex Generators[DOI]
Ramaswamy, Deepak Prem; Hinke, Rasmus; Schreyer, Anne-Marie
New Results in Numerical and Experimental Fluid Mechanics XII : Contributions to the 21st STAB/DGLR Symposium, Darmstadt, Germany, 2018 / edited by Andreas Dillmann, Gerd Heller, Ewald Krämer, Claus Wagner, Cameron Tropea, Suad Jakirlić 142 234-243 (2020)
Flow field around a spanwise-inclined jet in supersonic crossflow[DOI]
Sebastian, Robin; LĂĽrkens, Thomas; Schreyer, Anne-Marie
Aerospace science and technology 106 106209 (2020)
Correction: Experimental Investigation of Two Hypersonic Shock Turbulent Boundary Layer Interactions[DOI]
Schreyer, Anne-Marie; Sahoo, Dipankar; Williams, Owen J. H.; Smits, Alexander J.
AIAA journal 58-10 4613-4614 (2020)
Flow structure in the wake of a space-launcher model with propulsive-jet simulation[Open Access]
Schreyer, Anne-Marie
CEAS space journal 12-3 367-383 (2020)
2018
Experimental Investigation of Two Hypersonic Shock/Turbulent Boundary-Layer Interactions[DOI]
Schreyer, Anne-Marie; Sahoo, Dipankar; Williams, Owen J. H.; Smits, Alexander J.
AIAA journal 56-12 4830-4844 (2018)
2016
Analysis of acoustic and entropy disturbances in a hypersonic wind tunnel[DOI]
Schilden, Thomas; Schröder, Wolfgang; Ali, Syed Raza Christopher; Schreyer, Anne-Marie; Wu, Jie; Radespiel, Rolf
Physics of fluids 28-5 056104 (2016)