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:

Authors	Institution or Email of Authors	Author's ORCID iD
Sinha, Kautuk	kautuk.sinha (at) dlr.de	UNSPECIFIED
Klimmek, Thomas	thomas.klimmek (at) dlr.de	UNSPECIFIED
Schulze, Matthias	matthias.schulze (at) dlr.de	UNSPECIFIED
Handojo, Vega	Vega.Handojo (at) dlr.de	UNSPECIFIED

Date:

7 February 2021

Journal or Publication Title:

CEAS Aeronautical Journal

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Volume:

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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