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pCRM9 aeroelastic aircraft wing model for NASTRAN

dataset
posted on 25.10.2021, 08:09 authored by Paul LancelotPaul 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.

History

Publisher

4TU.ResearchData

Format

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

Organizations

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

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Licence

Exports