Finite element analysis of elements of aircraft structures
- Added: 20.03.2015
- Size: 4 MB
- Downloads: 0
Find out how to download this material
Subscribe to receive an information about new materials:
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.
Project's Content
|
diplom.docx
|
Similar materials
Free downloading for today
Update after: 6 hours 9 minutes
