Simulation of dynamic stall using direct-forcing immersed boundary method at low Reynolds number
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 2 August 2018
Issue publication date: 12 September 2018
Abstract
Purpose
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.
Design/methodology/approach
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.
Findings
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.
Practical implications
It is demonstrated that the DFIB model provides an accurate representation of dynamic stall phenomenon.
Originality/value
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.
Keywords
Citation
Vaziri, N., Chern, M.-J. and Horng, T.-L. (2018), "Simulation of dynamic stall using direct-forcing immersed boundary method at low Reynolds number", Aircraft Engineering and Aerospace Technology, Vol. 90 No. 5, pp. 869-876. https://doi.org/10.1108/AEAT-05-2017-0128
Publisher
:Emerald Publishing Limited
Copyright © 2018, Emerald Publishing Limited