Abstract:
Under consideration are the issues
of numerical solution of a boundary integral equation
describing the vorticity generation process
on the streamlined airfoils in meshless vortex methods.
The traditional approach based on the quadrature method
leads to the necessity of solving a system of linear algebraic equations
with dense matrix. If we consider the system of airfoils moving relative to one another,
this procedure has to be performed at each time step of the calculation,
and its high computational complexity significantly reduces
the efficiency of vortex methods.
The transition from the traditional approach
expressed by an integral equation of the first kind
to an approach with the integral equation of the second kind
makes it possible to apply the simple-iteration method
for numerical solving the boundary integral equation.
By examples of some model problems, we demonstrate that
the iterative approach allows reducing the computational
complexity of the problem
by tens to hundreds times while providing an acceptable
accuracy of the approximate solution.