Effect of suction and blowing control on NACA 0012 airfoil at low Reynolds number | Zendy

Zhiyong Zhang | Zendy; TuanTuan Wang | Zendy; Yafei Wang | Zendy; Hao Guo | Zendy

AI Assistant Blog Pricing

Home ZAIA Blog

Open Access

Effect of suction and blowing control on NACA 0012 airfoil at low Reynolds number

Author(s) -

Zhiyong Zhang,

TuanTuan Wang,

Yafei Wang,

Hao Guo

Publication year - 2020

Publication title -

journal of physics conference series

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.21

H-Index - 85

eISSN - 1742-6596

pISSN - 1742-6588

DOI - 10.1088/1742-6596/1600/1/012040

Subject(s) - airfoil , naca airfoil , mechanics , reynolds number , suction , drag , angle of attack , flow separation , lift (data mining) , materials science , physics , turbulence , aerodynamics , meteorology , computer science , data mining

To control the separation of flow past an airfoil with a simple jet mechanism, based on the Large Eddy Simulation from Favre, a suction-blowing combined jet is studied with holes placed on a NACA0012 airfoil’s upper surface and Re = 10 4 attack angle α = 6°. The results show the control mode of front-hole suction and back-hole blowing is effective. It can suppress the disturbance in the flow field and increase the lift-to-drag ratio of the airfoil at the same time.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.

Having issues? You can contact us here

Accelerating Research