Aerodynamic characteristics
of Pilatus PC-9
of Pilatus PC-9
In this paper word is given on calculation of aerodynamic coefficients and forces that are attacking the aircraft during his flight. Choosing the appropriate airfoils for wing and tail. Using proven methods for calculation of Lift, Drag and Pitching moment. Graphical presentation of results and their interpretation with elements of flight mechanics.
Lift force distribution on half of the wing span.
