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Modeling of CPACS-based fuselage structures using Python

Walther, Jan-Niclas and Petsch, Michael and Kohlgrüber, Dieter (2017) Modeling of CPACS-based fuselage structures using Python. Aircraft Engineering and Aerospace Technology, 89 (5), pp. 644-653. Emerald Group Publishing Ltd.. DOI: 10.1108/AEAT-01-2017-0043 ISSN 1748-8842

Full text not available from this repository.

Official URL: http://www.emeraldinsight.com/doi/full/10.1108/AEAT-01-2017-0028


Item URL in elib:https://elib.dlr.de/117525/
Document Type:Article
Title:Modeling of CPACS-based fuselage structures using Python
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Walther, Jan-NiclasJan-Niclas.Walther (at) dlr.deUNSPECIFIED
Petsch, MichaelMichael.Petsch (at) dlr.dehttps://orcid.org/0000-0002-2743-375X
Kohlgrüber, DieterDieter.Kohlgrueber (at) dlr.dehttps://orcid.org/0000-0002-6626-0927
Date:8 November 2017
Journal or Publication Title:Aircraft Engineering and Aerospace Technology
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:89
DOI :10.1108/AEAT-01-2017-0043
Page Range:pp. 644-653
Publisher:Emerald Group Publishing Ltd.
ISSN:1748-8842
Status:Published
Keywords:CPACS, Python, B-spline surfaces, Finite element model conversion, Fuselage structures, Preliminary aircraft design
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 - Simulation and Validation
Location: Hamburg
Institutes and Institutions:Institute of System Architectures in Aeronautics > Aircraft Design and System Integration
Institute of Structures and Design > Structural Integrity
Deposited By: Walther, Jan-Niclas
Deposited On:12 Jan 2018 11:41
Last Modified:06 Sep 2019 15:18

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