Load calculation of the fuselage
for Pilatus PC-9M aircraft
for Pilatus PC-9M aircraft
In this paper the word i s given to the stress calculation of the subjected fuselage according to rules and regulations stated in the EASA CS-23.
Results are shown via diagrams for moment and force. I've also made calculation of the
stringer of the fuselage who is on the critical position.
Results are shown via diagrams for moment and force. I've also made calculation of the
stringer of the fuselage who is on the critical position.
