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The numerical stress state analysis in the semi-monocoque fuselage

Bakunowicz J., Kopecki T.

Zeszyty Naukowe Politechniki Rzeszowskiej. Mechanika

2002

z. 58 [193]

37-44

In this paper stress state analysis in a semi-monocoque light transport aircraft fulselage is considered. The problem is supported with an example of threesectional fragment with a big hole. The numerical calculations are based on one of possible and defined in aviation requirements nonsymetrical, nonsteady-states of flight. Stress analysis was made by Finite Elements Method (FEM). The researches were concentrated on the neuralgic areas around the hole.