Sign In
 

​​​​

258
FLOWCON

 Catalog-Item Reuse ‭[2]‬

 Catalog-Item Reuse ‭[1]‬

FLOWCON - Flow Control

 

 

FLOWCON - Flow Control<img alt="" src="https://www.cira.it/PublishingImages/FLOWCON%201.jpg" style="BORDER:0px solid;" />https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/flowcon/FLOWCON - Flow ControlFLOWCON - Flow Control

 Media gallery

 

 

MLhttps://www.cira.it/PublishingImages/MLeXtra Large Eddy Simulation of a mixing layer. Isosurface of Q coloured by vorticityeXtra Large Eddy Simulation of a mixing layer. Isosurface of Q coloured by vorticityMLtext/html; charset=utf-8 Video<iframe src='https://www.youtube.com/embed/VRtLJTOYtY4' width='640' height='360' frameborder='0'></iframe>
Q_100_A5_UCOLOR_300https://www.cira.it/PublishingImages/Q_100_A5_UCOLOR_300Large eddy simulation of the incompressible flow around the NACA 0015 airfoil at Reynolds 3.0x105 and α=5°: Isosurface of Q coloured by streamwise velocityLarge eddy simulation of the incompressible flow around the NACA 0015 airfoil at Reynolds 3.0x105 and α=5°: Isosurface of Q coloured by streamwise velocityQ_100_A5_UCOLOR_300text/html; charset=utf-8 Video<iframe src='https://www.youtube.com/embed/yvC_HIjtsG4' width='640' height='360' frameborder='0'></iframe>
Q_100_EPPLER387_A07https://www.cira.it/PublishingImages/Q_100_EPPLER387_A07Large eddy simulation of the incompressible flow around the Eppler 387 airfoil at Reynolds 1.8x105 and α=7°: Isosurface of Q coloured by streamwise velocityLarge eddy simulation of the incompressible flow around the Eppler 387 airfoil at Reynolds 1.8x105 and α=7°: Isosurface of Q coloured by streamwise velocityQ_100_EPPLER387_A07text/html; charset=utf-8 Video<iframe src='https://www.youtube.com/embed/lHgPCgfC46M' width='640' height='360' frameborder='0'></iframe>
Q_100_naca0015_a10https://www.cira.it/PublishingImages/Q_100_naca0015_a10Large eddy simulation of the incompressible flow around the NACA 0015 airfoil at Reynolds 3.0x105 and α=10°: Isosurface of Q coloured by streamwise velocityLarge eddy simulation of the incompressible flow around the NACA 0015 airfoil at Reynolds 3.0x105 and α=10°: Isosurface of Q coloured by streamwise velocityQ_100_naca0015_a10text/html; charset=utf-8 Video<iframe src='https://www.youtube.com/embed/5A2BpEiODBw' width='640' height='360' frameborder='0'></iframe>
Q_100_SD7003_A12https://www.cira.it/PublishingImages/Q_100_SD7003_A12Large eddy simulation of the incompressible flow around the SD7003 airfoil at Reynolds 6.0x104 and α=12°: Isosurface of Q coloured by streamwise velocityLarge eddy simulation of the incompressible flow around the SD7003 airfoil at Reynolds 6.0x104 and α=12°: Isosurface of Q coloured by streamwise velocityQ_100_SD7003_A12text/html; charset=utf-8 Video<iframe src='https://www.youtube.com/embed/A651UoG0PDw' width='640' height='360' frameborder='0'></iframe>
Q_50_SD7003_A4https://www.cira.it/PublishingImages/Q_50_SD7003_A4Large eddy simulation of the incompressible flow around the SD7003 airfoil at Reynolds 6.0x104 and α=4°: Isosurface of Q coloured by streamwise velocityLarge eddy simulation of the incompressible flow around the SD7003 airfoil at Reynolds 6.0x104 and α=4°: Isosurface of Q coloured by streamwise velocityQ_50_SD7003_A4text/html; charset=utf-8 Video<iframe src='https://www.youtube.com/embed/L2DkWn24iIU' width='640' height='360' frameborder='0'></iframe>
Turbulence Modelling: eXtra Large Eddy Simulation. Spatially developing mixing layerhttps://www.cira.it/PublishingImages/Forms/DispForm.aspx?ID=2058Turbulence Modelling: eXtra Large Eddy Simulation. Spatially developing mixing layerTurbulence Modelling: eXtra Large Eddy Simulation. Spatially developing mixing layerImagehttps://www.cira.it/PublishingImages/FLOWCON%202.jpg
Turbulence Modelling: eXtra Large Eddy Simulation. Confluence of a boundary layer with a wakehttps://www.cira.it/PublishingImages/Forms/DispForm.aspx?ID=2057Turbulence Modelling: eXtra Large Eddy Simulation. Confluence of a boundary layer with a wakeTurbulence Modelling: eXtra Large Eddy Simulation. Confluence of a boundary layer with a wakeImagehttps://www.cira.it/PublishingImages/FLOWCON%203.jpg
Drag reduction: Skin friction coefficient over a wing-body configuration. Riblets applied on lower part of the figure https://www.cira.it/PublishingImages/Forms/DispForm.aspx?ID=2056Drag reduction: Skin friction coefficient over a wing-body configuration. Riblets applied on lower part of the figure Drag reduction: Skin friction coefficient over a wing-body configuration. Riblets applied on lower part of the figure Imagehttps://www.cira.it/PublishingImages/FLOWCON%204.jpg
Transition Modelling: Skin friction coefficient over a prolate spheroid https://www.cira.it/PublishingImages/Forms/DispForm.aspx?ID=2060Transition Modelling: Skin friction coefficient over a prolate spheroid Transition Modelling: Skin friction coefficient over a prolate spheroid Imagehttps://www.cira.it/PublishingImages/FLOWCON%205.jpg

 READ ALSO