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Effects of Antimetry on the Pro-Lattice Skin Inside Concept

Lohse-Busch, Heike (2013) Effects of Antimetry on the Pro-Lattice Skin Inside Concept. Other. DLR-Interner Bericht. DLR-IB 131-2013/12, 27 S.

Full text not available from this repository.

Abstract

In the scope of the ALaSCA project, a carbon fiber composite grid-type structure, called anisogrid structure, is investigated for the use in aircraft fuselages. The novel structural design presents two striking differences when compared to the traditional aircraft fuselage design: 1) the stiffening elements form a grid with non-rectangular skin bays, 2) grid stiffening elements are located on the inside as well as on the outside of the skin creating an antimetric structure. The unusual arrangement of stiffeners on either side of the skin leads to a difference in load carried by the inner and the outer stiffeners, which in turn could lead to an adverse structural response. The goal of the study presented in this report is to determine whether antimetry causes flight safety critical structural responses in the developed design.

Item URL in elib:https://elib.dlr.de/84342/
Document Type:Monograph (DLR-Interner Bericht, Other)
Title:Effects of Antimetry on the Pro-Lattice Skin Inside Concept
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lohse-Busch, HeikeUNSPECIFIEDUNSPECIFIED
Date:January 2013
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:27
Status:Published
Keywords:Anisogrid, Antimetry, Composite Fuselage, FEM, ALaSCA
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:04 Nov 2013 08:33
Last Modified:04 Nov 2013 08:33

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