Source term model for rod vortex generator
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 17 October 2018
Issue publication date: 17 September 2019
Abstract
Purpose
The simulations of grid-resolved rod vortex generators (RVGs) require high computational cost and time. Additionally, the computational mesh topology must be adjusted to rods geometries. The purpose of this study is to propose the new source term model for RVG.
Design/methodology/approach
The model was proposed by modification of Bender, Anderson, Yagle (BAY) model used to predict flows around different type of vortex generators (VGs) – vanes. Original BAY model was built on lifting line theory. The proposed model was implemented in ANSYS Fluent by means of the user-defined function technique. Additional momentum and energy sources are imposed to transport equations.
Findings
The computational results of source term model were validated against experimental data and numerical simulation results for grid-resolved rod. It was shown that modified BAY model can be successfully used for RVG in complex cases. An example of BAY model application for RVG on transonic V2C airfoil with strongly oscillating shock waves is presented. Aerodynamic performance predicted numerically by means of both approaches (grid resolved RVG and modeled) is in good agreement, what indicates application opportunity of the proposed model to complex cases.
Practical implications
Modified BAY model can be used to simulate the influence of RVGs in complex real cases. It allows for time/cost reduction if the location or distribution of RVG has to be optimized on a profile, wing or in the channel.
Originality/value
In the paper, the new modification of BAY model was proposed to simulate RVGs. The presented results are innovative because of original approach to model RVGs.
Keywords
Citation
Kwiatkowski, T., Flaszyński, P. and Zoltak, J. (2019), "Source term model for rod vortex generator", Aircraft Engineering and Aerospace Technology, Vol. 91 No. 9, pp. 1169-1179. https://doi.org/10.1108/AEAT-01-2018-0072
Publisher
:Emerald Publishing Limited
Copyright © 2018, Emerald Publishing Limited