Simulation of a Maneuvering Aircraft Using a Panel Method
P Schoř, M Kouřil, V Daněk - Acta Polytechnica, 2021 - ojs.cvut.cz
We present a method for numerical simulations of a maneuvering aircraft, which uses a first-
order unsteady panel method as the only source of aerodynamic forces and moments. By …
order unsteady panel method as the only source of aerodynamic forces and moments. By …
Aerodynamic load of an aircraft with a highly elastic wing
P Schoř - 2017 - dspace.cvut.cz
In this article, a method for calculation of air loads of an aircraft with an elastic wing is
presented. The method can predict a redistribution of air loads when the elastic wing …
presented. The method can predict a redistribution of air loads when the elastic wing …