1: Introduction
The program FLZ-Vortex is used to examine the distribution of forces and
momenta of complex airplane constructions. The airplane construction is set up
by means of a 3D-editor.
For computations the Vortex-Lattice-Method VLM is applied.
In contrast to
As with the aforementioned methods VLM uses the airfoil's mean camber line for
computation. At first airfoil thickness and viscous influence (skin-friction)
are not taken into account.