LES of synthetic jets in boundary layer with laminar separation caused by adverse pressure gradient

DOI10.1016/J.COMPFLUID.2009.12.012zbMath1242.76081OpenAlexW1983145643MaRDI QIDQ435622

Tetsuya Ozawa, Guang Hong, Samuel Lesbros

Publication date: 11 July 2012

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/10453/13526

zbMATH Keywords

numerical modelingflow controlmicro sensorsynthetic jet actuator

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65) Turbulent boundary layers (76F40)

Related Items (5)

The interaction of round synthetic jets with a turbulent boundary layer separating from a rounded ramp ⋮ Characterization of flow vectoring phenomenon in adjacent synthetic jets using CFD and PIV ⋮ Comparative study of boundary layer control around an ordinary airfoil and a high lift airfoil with secondary blowing ⋮ Numerical prediction of turbulent flow structure generated by a synthetic cross‐jet into a turbulent boundary layer ⋮ Active control of flow over a rounded ramp by means of single and double adjacent rectangular synthetic jet actuators

Cites Work

• Unnamed Item
• On the virtual aeroshaping effect of synthetic jets
• Direct numerical simulation of ‘short’ laminar separation bubbles with turbulent reattachment
• Flow Control
• S<scp>YNTHETIC</scp> J<scp>ETS</scp>

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