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Development and Validation of a Parametric Finite Element Model for the Spar - Skin Joint of a Carbon Fiber Reinforced Polymer Wing

Gesell, Thomas Manfred and Bach, Tobias (2018) Development and Validation of a Parametric Finite Element Model for the Spar - Skin Joint of a Carbon Fiber Reinforced Polymer Wing. Master's. DLR-Interner Bericht. DLR-IB-FA-BS-2018-224, 115 S.

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Item URL in elib:https://elib.dlr.de/125765/
Document Type:Monograph (DLR-Interner Bericht, Master's)
Title:Development and Validation of a Parametric Finite Element Model for the Spar - Skin Joint of a Carbon Fiber Reinforced Polymer Wing
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gesell, Thomas ManfredUniversität StuttgartUNSPECIFIED
Bach, Tobiastobias.bach (at) dlr.deUNSPECIFIED
Date:November 2018
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:115
Status:Published
Keywords:Structural Design, Composites, Structural Optimization, skin-spar joint
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures and Materials
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures
Deposited By: Böhringer-Thelen, Isolde
Deposited On:11 Jan 2019 08:06
Last Modified:03 May 2019 11:09

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