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Unsteady flow organisation of shock-wave/boundary-layer interactions controlled with air-jet vortex generators
Mapping Intimacies
◽
10.2514/6.2022-0700
◽
2022
◽
Author(s):
Deepak Prem Ramaswamy
◽
Anne-Marie Schreyer
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Unsteady Flow
◽
Vortex Generators
◽
Wave Boundary Layer
◽
Air Jet
◽
Wave Boundary
Download Full-text
Related Documents
Cited By
References
Effect of air jet vortex generators on a shock wave boundary layer interaction
Experiments in Fluids
◽
10.1007/s00348-010-0854-8
◽
2010
◽
Vol 49
(5)
◽
pp. 1053-1064
◽
Cited By ~ 55
Author(s):
L. J. Souverein
◽
J.-F. Debiève
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Vortex Generators
◽
Layer Interaction
◽
Wave Boundary Layer
◽
Air Jet
◽
Boundary Layer Interaction
◽
Wave Boundary
Download Full-text
Effect on a shock wave boundary layer interaction of air jet vortex generators
Progress in Flight Physics
◽
10.1051/eucass/201203141
◽
2012
◽
Cited By ~ 1
Author(s):
L. J. Souverein
◽
J.-F. Debiève
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Vortex Generators
◽
Layer Interaction
◽
Wave Boundary Layer
◽
Air Jet
◽
Boundary Layer Interaction
◽
Wave Boundary
Download Full-text
Micro-vortex generators for shock wave/boundary layer interactions
Progress in Aerospace Sciences
◽
10.1016/j.paerosci.2014.12.006
◽
2015
◽
Vol 74
◽
pp. 16-47
◽
Cited By ~ 41
Author(s):
Argyris G. Panaras
◽
Frank K. Lu
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Vortex Generators
◽
Wave Boundary Layer
◽
Wave Boundary
Download Full-text
Control of a Shock-Wave/Boundary-Layer Interaction and Subsequent Subsonic Diffuser Using a Combination of Vortex Generators and Bleed
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
◽
10.2514/6.2012-274
◽
2012
◽
Cited By ~ 5
Author(s):
Neil Titchener
◽
Holger Babinsky
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Vortex Generators
◽
Layer Interaction
◽
Wave Boundary Layer
◽
Boundary Layer Interaction
◽
Subsonic Diffuser
◽
Wave Boundary
Download Full-text
Shock-Wave Boundary-Layer Interaction Control on a Compression Corner Using Mechanical Vortex Generators
28th International Symposium on Shock Waves
◽
10.1007/978-3-642-25685-1_62
◽
2012
◽
pp. 409-415
◽
Cited By ~ 1
Author(s):
C. Manisankar
◽
S. B. Verma
◽
C. Raju
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Vortex Generators
◽
Layer Interaction
◽
Wave Boundary Layer
◽
Interaction Control
◽
Compression Corner
◽
Boundary Layer Interaction
◽
Wave Boundary
Download Full-text
Shock Wave/Boundary-Layer Interaction Control Using a Combination of Vortex Generators and Bleed
AIAA Journal
◽
10.2514/1.j052079
◽
2013
◽
Vol 51
(5)
◽
pp. 1221-1233
◽
Cited By ~ 38
Author(s):
Neil Titchener
◽
Holger Babinsky
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Vortex Generators
◽
Layer Interaction
◽
Wave Boundary Layer
◽
Interaction Control
◽
Boundary Layer Interaction
◽
Wave Boundary
Download Full-text
Shock Wave Boundary Layer Interaction Control by Rod Vortex Generators
30th International Symposium on Shock Waves 2
◽
10.1007/978-3-319-44866-4_60
◽
2017
◽
pp. 1135-1139
Author(s):
R. Szwaba
◽
P. Doerffer
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Vortex Generators
◽
Layer Interaction
◽
Wave Boundary Layer
◽
Interaction Control
◽
Boundary Layer Interaction
◽
Wave Boundary
Download Full-text
Vortex Generators for Corner Separation Caused by Shock-Wave/Boundary-Layer Interactions
Journal of Aircraft
◽
10.2514/1.c034994
◽
2019
◽
Vol 56
(1)
◽
pp. 239-249
◽
Cited By ~ 1
Author(s):
Shunsuke Koike
◽
Holger Babinsky
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Vortex Generators
◽
Corner Separation
◽
Wave Boundary Layer
◽
Wave Boundary
Download Full-text
Effect of Vortex Generators on Corner Flow Separation Caused by Shock Wave-Boundary-Layer Interaction
2018 AIAA Aerospace Sciences Meeting
◽
10.2514/6.2018-1811
◽
2018
◽
Author(s):
Shunsuke Koike
◽
Holger Babinsky
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Flow Separation
◽
Vortex Generators
◽
Layer Interaction
◽
Wave Boundary Layer
◽
Corner Flow
◽
Boundary Layer Interaction
◽
Wave Boundary
Download Full-text
SHOCK WAVE BOUNDARY LAYER INTERACTION INVESTIGATION: CONTROL BY ROD VORTEX GENERATORS AND THEIR APPLICATION ON HELICOPTER ROTOR BLADES
Proceedings of the VII European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS Congress 2016)
◽
10.7712/100016.1901.11983
◽
2016
◽
Author(s):
Fernando Tejero Embuena
◽
Piotr Doerffer
◽
Pawel Flaszynski
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Rotor Blades
◽
Vortex Generators
◽
Helicopter Rotor
◽
Layer Interaction
◽
Wave Boundary Layer
◽
Helicopter Rotor Blades
◽
Boundary Layer Interaction
◽
Wave Boundary
Download Full-text
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