The doi above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
doi: 10.4121/984090ea-26fd-4809-8dac-f41367bf8916

Carrillo Córcoles, Xavier; de Breuker, Roeland; Sodja, Jurij (2024): M001 - GVT Data and Nastran models (August 2024) (Models based on the publication: Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads). Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/984090ea-26fd-4809-8dac-f41367bf8916.v1

Dataset

• Aerospace Transport
• Transport

Aeroelastic Tailoring, FE Model Update, Finite Element Models, Flared Folding Wingtips, Ground Vibration Tests

CC BY 4.0

• Flared Folding Wingtips - TU Delft

RefWorks, BibTeX, Reference Manager, Endnote, DataCite, NLM, DC, CFF

by Xavier Carrillo Córcoles , Roeland de Breuker , Jurij Sodja

GVT Data and Nastran models of five wings with a flared folding wingtip, featuring different stiffness properties.

The GVT data is the modal test input file automatically generated by NX/Simcenter when importing modal data from Simcenter TestLab. It contains the position of the sensors and the different mode shapes

The Nastran models are based on the models of the original publication but have been generated using different modelling techniques. These new models (Original) are updated using the model update procedure in Simcenter to achieve better correlation with the GVT data (Updated).

• 2024-08-12 first online, published, posted

4TU.ResearchData

.zip file containing GVT data saved in .unv files, Simulation files saved in .dat files and Mode Shape images saved as .png.

Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads

TU Delft, Faculty of Aerospace Engineering, Department of Aerospace Structures & Materials