The effects of Mach number on the flow separation control of airfoil with a small plate near the leading edge

DOI10.1016/j.compfluid.2017.07.014zbMath1390.76268OpenAlexW2735239545MaRDI QIDQ1648458

Diangui Huang, Longfeng Hou, Yangwei Zhou

Publication date: 27 June 2018

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

Full work available at URL: https://doi.org/10.1016/j.compfluid.2017.07.014

zbMATH Keywords

Mach numberairfoilnumerical studyflow separation control

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) (k)-(varepsilon) modeling in turbulence (76F60) General aerodynamics and subsonic flows (76G25)

Related Items (1)

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Cites Work

• Two-dimensional turbulent viscous flow simulation past airfoils at fixed incidence
• Mechanism of Roe-type schemes for all-speed flows and its application
• Distributed forcing of flow over a circular cylinder
• All-speed Roe scheme for the large eddy simulation of homogeneous decaying turbulence

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