Numerical simulation and experiments on turbulent air flow around the semi-circular profile at zero angle of attack and moderate Reynolds number-Reference-Cited by-同舟云学术

Numerical simulation and experiments on turbulent air flow around the semi-circular profile at zero angle of attack and moderate Reynolds number

Published:2019-06 Issue: Volume:188 Page:1-17
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Isaev Sergey^ORCID,Baranov Paul,Popov Igor,Sudakov Alexander,Usachov Alexander,Guvernyuk Sergey,Sinyavin Alexei,Chulyunin Alexei,Mazo Alexander,Demidov Dennis,Dekterev Alexander,Gavrilov Andrey,Shebelev Alexander

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

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3. Analysis of extremal lift behavior of a semi-circular airfoil in a turbulent airfoil at a near-zero angle of attack;Isaev;Techn Phys Letters,2015

4. A. Savitsky, L. Schukin, V. Karelin et al., Method for control of the boundary layer on the aerodynamic surface of an aircraft, and the aircraft provided with the boundary layer control system. United States Patent No. 5417391, 1995.

5. Controlling the turbulent flow past a thick airfoil by means of flow enhancement in vortex cells using suction from central body surfaces;Baranov;Fluid Dyn,2003

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