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Skin Panel Optimization of the Common Research Model Wing Using Sandwich Composites

Meddaikar, Muhammad Yasser and Dillinger, Johannes and Silva Caprio, Gustavo and De Breuker, Roeland (2021) Skin Panel Optimization of the Common Research Model Wing Using Sandwich Composites. Journal of Aircraft. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C036551. ISSN 0021-8669.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/full/10.2514/1.C036551


Item URL in elib:https://elib.dlr.de/145668/
Document Type:Article
Title:Skin Panel Optimization of the Common Research Model Wing Using Sandwich Composites
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Meddaikar, Muhammad YasserMuhammad.Meddaikar (at) dlr.dehttps://orcid.org/0000-0001-9580-7023
Dillinger, JohannesJohannes.Dillinger (at) dlr.dehttps://orcid.org/0000-0002-7522-7555
Silva Caprio, GustavoGustavo.Silva (at) dlr.deUNSPECIFIED
De Breuker, RoelandAerospace Structures, Delft University of Technologyhttps://orcid.org/0000-0002-7882-2173
Date:2021
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.2514/1.C036551
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0021-8669
Status:Published
Keywords:Composite optimization, Sandwich composites, Lamination parameters
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: Meddaikar, Muhammad Yasser
Deposited On:02 Dec 2021 15:55
Last Modified:02 Dec 2021 15:55

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