Finite element analysis of elements of aircraft structures
- Added: 20.03.2015
- Size: 4 MB
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Description
The object of the study of this work is the stop of the working door of the fuselage of the MS-21-300 aircraft, which is attached to the hull using four bolts.
2 tasks are considered: linear and taking into account contact.
The construction of the finite element model and the necessary calculations are carried out in the Femap program.
2 tasks are considered: linear and taking into account contact.
The construction of the finite element model and the necessary calculations are carried out in the Femap program.
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diplom.docx
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