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Evolution and Evaluation of Anisogrid Fuselage Barrel Concepts

Pinier, Thibaut (2012) Evolution and Evaluation of Anisogrid Fuselage Barrel Concepts. DLR-Interner Bericht. DLR-IB 131-2012/58. Master's. 81 S. (Unpublished)

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The purpose of the project is to determine the behaviours of a grid stiffened fuselage structure under pure and combined loads. The influence of anisotropy, geomety, and material parameters on the response of the structure was studied. CLT, smearing method, and FEM with parametric session file (MSC) were used. Design recommendations were formulated to minimize unwanted structural responses and decrease weight while respecting strnegth and stiffness criteria.

Item URL in elib:https://elib.dlr.de/84501/
Document Type:Monograph (DLR-Interner Bericht, Master's)
Title:Evolution and Evaluation of Anisogrid Fuselage Barrel Concepts
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Date:September 2012
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:81
Keywords:Grid, grid stiffened, anisogrid, lattice, anisotropic, anisotropy, CLT, FEM, smearing method, parametric session file, fuselage, composite, structural behavior
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures & Materials (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures
Deposited By: Böhringer-Thelen, Isolde
Deposited On:11 Nov 2013 20:12
Last Modified:11 Nov 2013 20:12

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