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: 10.4121/16834387

Lancelot, Paul (2021): pCRM9 aeroelastic aircraft wing model for NASTRAN. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/16834387.v1

Dataset

• Aerospace Engineering

Aeroelasticity, aircraft wings, Finite Elements, Nastran

CC BY 4.0

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

by Paul Lancelot

This is the pCRM9 aeroelastic finite element model. It is based on the University of Michigan undeflected CRM geometry (uCRM). This FEM model is tailored for optimisation and load analysis using NASTRAN.

• 2021-10-25 first online, published, posted

4TU.ResearchData

Text (.bdf .dat and .txt) and Image (.png)

pCRM9 aeroelastic model for NASTRAN

• https://data.mendeley.com/datasets/gpk4zn73xn/1

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