pCRM9 aeroelastic aircraft wing model for NASTRAN

doi: 10.4121/16834387.v1
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
Datacite citation style:
Lancelot, Paul (2021): pCRM9 aeroelastic aircraft wing model for NASTRAN. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/16834387.v1
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite
Dataset
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licence
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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.
history
  • 2021-10-25 first online, published, posted
publisher
4TU.ResearchData
format
Text (.bdf .dat and .txt) and Image (.png)
associated peer-reviewed publication
pCRM9 aeroelastic model for NASTRAN
organizations
TU Delft, Faculty of Aerospace Engineering, Department of Aerospace Structures and Materials

DATA

files (10)