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Loads analysis and structural optimization of a high aspect ratio composite wing aircraft

Sinha, Kautuk and Klimmek, Thomas and Schulze, Matthias and Handojo, Vega (2021) Loads analysis and structural optimization of a high aspect ratio composite wing aircraft. CEAS Aeronautical Journal, 12, pp. 233-243. Springer. doi: 10.1007/s13272-021-00494-x. ISSN 1869-5590.

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Official URL: https://link.springer.com/article/10.1007/s13272-021-00494-x


Item URL in elib:https://elib.dlr.de/142177/
Document Type:Article
Title:Loads analysis and structural optimization of a high aspect ratio composite wing aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Sinha, Kautukkautuk.sinha (at) dlr.deUNSPECIFIED
Klimmek, Thomasthomas.klimmek (at) dlr.deUNSPECIFIED
Schulze, Matthiasmatthias.schulze (at) dlr.deUNSPECIFIED
Handojo, VegaVega.Handojo (at) dlr.deUNSPECIFIED
Date:7 February 2021
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:12
DOI:10.1007/s13272-021-00494-x
Page Range:pp. 233-243
Publisher:Springer
ISSN:1869-5590
Status:Published
Keywords:composite wing, structural optimization, manoeuvre load alleviation, high aspect ratio wing, aeroelastic load computation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Aircraft Technologies and Integration
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Sinha, Kautuk
Deposited On:26 Aug 2021 16:37
Last Modified:26 Aug 2021 16:37

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