The purpose of this study is simulation of dynamic stall behavior around the Eppler 387 airfoil in the low Reynolds number flow with a direct-forcing immersed boundary (DFIB) numerical model.
A ray-casting method is used to define the airfoil geometry. The governing continuity and Navier–Stokes momentum equations and boundary conditions are solved using the DFIB method.
The purposed method is validated against numerical results from alternative schemes and experimental data on static and oscillating airfoil. A base flow regime and different vortices patterns are observed, in accordance with other previously published investigations. Also, the effects of the reduced frequency, the pitch oscillation amplitude and the Reynolds number are studied. The results show that the reduced frequency has a major effect on the flow field and the force coefficients of the airfoil. On the other hand, the Reynolds number of the flow has a little effect on the dynamic stall characteristics of the airfoil at least in the laminar range.
It is demonstrated that the DFIB model provides an accurate representation of dynamic stall phenomenon.
The results show that the dynamic stall behavior around the Eppler 387 is different than the general dynamic stall behavior understanding in the shedding phase.
Simulation of dynamic stall using direct-forcing immersed boundary method at low Reynolds number
Aircraft Engineering and Aerospace Technology ; 90 , 5 ; 869-876
2018-08-02
8 pages
Article (Journal)
Electronic Resource
English
SIMULATION OF THE DYNAMIC STALL AT LOW REYNOLDS NUMBER
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