The calculations described were carried out for an F28-Mk 1000 C aircraft with a large cargo door. Using the ASKA program system, based on the finite element method, a great part of the fuselage, embedding the wingbox connection and the adjacent cargo door, was divided into about 3000 elements of different types: membrane and beam elements. Two loading cases, a cabine pressure case, and a fuselage bending case were considered. Results of calculations are compared with results of measurements on the structure.
Calculation of Strength and Stiffness of an Aeroplane Fuselage Part with a Large Cargo Door
1976
73 pages
Report
No indication
English
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