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Robin Sebastian
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Flow field around a spanwise-inclined jet in supersonic crossflow
R Sebastian, T Lürkens, AM Schreyer
Aerospace Science and Technology 106, 106209, 2020
302020
Numerical simulation of a turbulent channel flow with an acoustic liner
R Sebastian, D Marx, V Fortuné
Journal of Sound and Vibration 456, 306-330, 2019
262019
Influence of jet spacing in spanwise-inclined jet injection in supersonic crossflow
R Sebastian, AM Schreyer
Journal of Fluid Mechanics 946, A39, 2022
142022
Flow fields around spanwise-inclined elliptical jets in supersonic crossflow
R Sebastian, AM Schreyer
European Journal of Mechanics-B/Fluids 94, 299-313, 2022
122022
Control of SWBLI in a 24deg Compression Ramp Flow with Air-jet Vortex-generator
R Sebastian, AM Schreyer
AIAA Scitech 2023 Forum, 2138, 2023
112023
Spanwise-inclined jets in supersonic crossflow: effects of injection pressure and separation-control effectiveness
R Sebastian, DP Ramaswamy, AM Schreyer
AIAA Journal 61 (9), 3833-3847, 2023
102023
Influence of crossflow Mach number on spanwise-inclined jet injection
R Sebastian, AM Schreyer
AIAA Scitech 2022 Forum, 1363, 2022
92022
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
92021
Numerical simulation of a compressible channel flow with an acoustic liner
R Sebastian, D Marx, V Fortuné, E Lamballais
23rd AIAA/CEAS Aeroacoustics Conference, 4034, 2017
72017
Forced injection of a spanwise-inclined jet in supersonic crossflow
R Sebastian, AM Schreyer
AIAA Journal 62 (1), 52-64, 2024
32024
Effects of jet-injection-pipe length on the flow-control effectiveness of spanwise-inclined jets in supersonic crossflow
DP Ramaswamy, R Sebastian, AM Schreyer
Physical Review Fluids 8 (11), 113902, 2023
32023
Forced Control of SWBLI in a 24deg Compression Ramp Flow with Air-jet Vortex-generator
R Sebastian, AM Schreyer
AIAA AVIATION 2023 Forum, 4238, 2023
32023
Spatial Numerical Simulation of a Turbulent Plane Channel Flow with an Impedance Wall
D Marx, R Sebastian, V Fortune
25th AIAA/CEAS Aeroacoustics Conference, 2543, 2019
32019
Numerical simulation of acoustic propagation in a turbulent spatial channel flow with acoustic liner
R Sebastian, D Marx, V Fortuné
EFMC 12, 2018
22018
Numerical simulation of a compressible channel flow with impedance boundary condition
R Sebastian, D Marx, V Fortuné, E Lamballais
New challenges in Wall Turbulence, 2017
22017
Flow fields around asymmetrical micro vortex generators in supersonic flow
L Hristozova, R Sebastian, AM Schreyer
Aerospace Science and Technology 145, 108838, 2024
12024
Spanwise-inclined injection of unsteady jets in supersonic crossflow
R Sebastian, AM Schreyer
AIAA AVIATION 2022 Forum, 3853, 2022
12022
Numerical simulation of acoustic propagation in a turbulent channel flow with an acoustic liner
R Sebastian
University of Poitiers, 2018
12018
Design considerations for efficient spanwise-inclined air-jet vortex generators for separation control in supersonic and hypersonic flows
R Sebastian, AM Schreyer
Aerospace Science and Technology 147, 109033, 2024
2024
Simulation of instability and sound production in a turbulent channel flow with an acoustic liner
D Marx, R Sebastian, V Fortuné
Journal of Sound and Vibration 573, 118223, 2024
2024
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