Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media
Source abstract
Abstract
In this paper, the boundary element method is applied to determine the characteristics of distributed flow around the airfoil group. Because the boundary integral equation can describe various initial boundary value problems in mechanics and has many advantages such as good convergence, it can be used as a tool to establish appropriate mathematical models and numerical realization methods, so as to comprehensively study the distribution kinematics and dynamics of the airfoil group motion system in the viscous fluid flow co-flow process. In this paper, some numerical results are presented to determine the aerodynamic distribution characteristics of the viscous flow field around the airfoil group in the control area.
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Research context
OpenAlex topics: Numerical methods in engineering · Advanced Numerical Methods in Computational Mathematics · Lattice Boltzmann Simulation Studies
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