Structural Analysis Of Fuselage With Lattice Structure

Structural Analysis Of Fuselage With Lattice Structure
Authors : B. Karthick, S. Balaji, P. Maniiarasan
Publication Date: 20-06-2013


Author(s):  B. Karthick, S. Balaji, P. Maniiarasan

Published in:   International Journal of Engineering Research & Technology

License:  This work is licensed under a Creative Commons Attribution 4.0 International License.

Website: www.ijert.org

Volume/Issue:   Vol.2 - Issue 6 (June - 2013)

e-ISSN:   2278-0181


The design of a fuselage structure for any aircraft is very essential. The fuselage structure for business jet aircraft carries stringers, frames, floor beam and outer skin. The fuselage structure for heavy passenger aircraft carries a wide numerous structural parts such as bulkheads, longerons, frames, stringers, flat plate, outer skin etc. Nowadays, stiffened shell structure was used in fuselage structure. The lattice structure is a complex design which carries a individual structural components of actual fuselage structure seen. In this project, the lattice structure was adapted to the aircraft instead of stiffened shell structure. The design of the lattice structure is carried out in CATIA and the static structural analysis is carried out in ANSYS to find the stress and deformation due to the load.


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