Comparative study of boundary layer control around an ordinary airfoil and a high lift airfoil with secondary blowing

DOI10.1016/J.COMPFLUID.2017.03.012zbMath1390.76258OpenAlexW2593255934MaRDI QIDQ1649639

Sandeep Eldho James, Jiss J. Sebastian, Heuy Dong Kim, Abhilash Suryan, Abhay Mohan

Publication date: 28 June 2018

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

Full work available at URL: https://doi.org/10.1016/j.compfluid.2017.03.012

zbMATH Keywords

lift coefficientboundary layer controlblowing ratiosecondary blowingstall delay

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Software, source code, etc. for problems pertaining to fluid mechanics (76-04)

Cites Work

• Normal shock boundary layer control with various vortex generator geometries
• Numerical study of passive and active flow separation control over a NACA0012 airfoil
• LES of synthetic jets in boundary layer with laminar separation caused by adverse pressure gradient
• Coupling active and passive techniques to control the flow past the square back ahmed body
• Direct numerical simulation of flow separation around NACA 0012 airfoil
• DNS for flow separation control around an airfoil by pulsed jets
• The numerical computation of turbulent flows
• Trailing‐edge separation control on an aerofoil in low‐speed flow
• Passive control of the flow around a square cylinder using porous media

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