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Anne-Marie Schreyer
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Particle response analysis for particle image velocimetry in supersonic flows
OJH Williams, T Nguyen, AM Schreyer, AJ Smits
Physics of Fluids 27 (7), 076101, 2015
432015
Analysis of acoustic and entropy disturbances in a hypersonic wind tunnel
T Schilden, W Schröder, SRC Ali, AM Schreyer, J Wu, R Radespiel
Physics of Fluids 28 (5), 056104, 2016
222016
Flow field around a spanwise-inclined jet in supersonic crossflow
R Sebastian, T Lürkens, AM Schreyer
Aerospace Science and Technology 106, 106209, 2020
142020
Experimental investigations of a hypersonic shock turbulent boundary layer interaction
AM Schreyer, D Sahoo, A Smits
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011
142011
Influence of jet spacing and injection pressure on separation control with air-jet vortex generators
DP Ramaswamy, R Hinke, AM Schreyer
Symposium der Deutsche Gesellschaft für Luft-und Raumfahrt, 234-243, 2018
132018
Experiments on the influence of a microramp array on a hypersonic shock turbulent boundary layer interaction
AM Schreyer, D Sahoo, A Smits
41st AIAA Fluid Dynamics Conference and Exhibit, 3428, 2011
132011
Destination Moon and beyond for the Microrover Nanokhod
S Klinkner, CGY Lee, C Wagner, W Hlawatsch, AM Schreyer, HP Röser
Deutsche Gesellschaft für Luft-und Raumfahrt-Lilienthal-Oberth eV, Bonn, 2007
132007
Control of shock-induced separation of a turbulent boundary layer using air-jet vortex generators
DP Ramaswamy, AM Schreyer
AIAA Journal 59 (3), 927-939, 2021
112021
Development of a Dual-PIV system for high-speed flow applications
AM Schreyer, JJ Lasserre, P Dupont
Experiments in Fluids 56 (10), 1-12, 2015
112015
Velocity spectrum estimation in shock-wave/turbulent boundary-layer interaction
T Jiang, AM Schreyer, L Larchevêque, S Piponniau, P Dupont
AIAA Journal 55 (10), 3486-3498, 2017
102017
Turbulence measurements with PIV in a hypersonic shock boundary layer interaction
AM Schreyer, D Sahoo, A Smits
41st AIAA Fluid Dynamics Conference and Exhibit, 3429, 2011
102011
Experimental Investigation of Two Hypersonic Shock/Turbulent Boundary-Layer Interactions
AM Schreyer, D Sahoo, OJH Williams, AJ Smits
AIAA Journal 56 (12), 4830-4844, 2018
92018
Method for spectra estimation from high-speed experimental data
AM Schreyer, L Larchevêque, P Dupont
AIAA Journal 54 (2), 557-568, 2016
82016
Characterization of the supersonic wake of a generic space launcher
AM Schreyer, S Stephan, R Radespiel
CEAS Space Journal 9 (1), 97-110, 2017
72017
Effect of jet spacing in separation control with air jet vortex generators
DP Ramaswamy, AM Schreyer
AIAA Scitech 2019 Forum, 1653, 2019
62019
Design of a high-speed focusing schlieren system for complex three-dimensional flows
C Schauerte, AM Schreyer
5th International Conference on Experimental Fluid Mechanics (ICEFM 2018 …, 2018
62018
Separation control in a hypersonic compression ramp interaction
AM Schreyer, I Bermejo-Moreno, J Kim, J Urzay
Proceedings of the Summer Program, 223, 2016
52016
Influence of air-jet stability on the flow-control effectiveness of air-jet vortex generators
DP Ramaswamy, R Sebastian, AM Schreyer
APS Division of Fluid Dynamics Meeting Abstracts, Q21. 004, 2021
42021
LES of hypersonic compression-corner flows with upstream sub-boundary-layer microramp vortex generators
J Kim, I Bermejo-Moreno, AM Schreyer, J Urzay
Center for Turbulence Research Annual Research Briefs, 2016
42016
Effects of Jet-to-Jet Spacing of Air-Jet Vortex Generators in Shock-Induced Flow-Separation Control
DP Ramaswamy, AM Schreyer
Flow, Turbulence and Combustion, 1-30, 2022
32022
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Articles 1–20