Publications
Publications of "schreyer, a."
2024
Shock Oscillation Mechanism of Highly Separated Transitional Shock-Wave/Boundary-Layer Interactions[DOI]
AIAA journal 1-13 (2024)
AIAA journal 1-13 (2024)
Influences in Experimental Studies on the Characteristics of Transonic Shock Buffet[DOI]
AIAA journal [1]-17 (2024)
AIAA journal [1]-17 (2024)
Highly separated transitional shock-wave/boundary-layer interactions: A spatial modal study[DOI]
Physics of fluids 36-11 116114 (2024)
Physics of fluids 36-11 116114 (2024)
Effect of Transition on Self-Sustained Shock Oscillations in Highly Loaded Transonic Rotors[DOI]
AIAA journal 62-6 2063-2075 (2024)
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[DOI]
Aerospace science and technology 147 109033 (2024)
Aerospace science and technology 147 109033 (2024)
2023
Control of shock-induced flow separation with Air-Jet vortex generators[Open Access]
(Schreyer, Anne-Marie; Schröder, Wolfgang; Sandham, Neil)
PhD Thesis (2023)
(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]
Physical review fluids 8-11 113902 (2023)
Physical review fluids 8-11 113902 (2023)
Numerical analysis of the flow around a speed skydiver[DOI]
European journal of mechanics / B 100 163-178 (2023)
European journal of mechanics / B 100 163-178 (2023)
Effects of favourable downstream pressure gradients on separated shock-wave/boundary-layer interactions[DOI]
The international journal of heat and fluid flow 102 109164 (2023)
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]
AIAA journal 61-9 3833-3847 (2023)
AIAA journal 61-9 3833-3847 (2023)
2022
Influence of jet spacing in spanwise-inclined jet injection in supersonic crossflow[DOI]
Journal of fluid mechanics 946 A39 (2022)
Journal of fluid mechanics 946 A39 (2022)
2021
2020
Flow field around a spanwise-inclined jet in supersonic crossflow[DOI]
Aerospace science and technology 106 106209 (2020)
Aerospace science and technology 106 106209 (2020)