%0 Generic
%A Lancelot, Paul
%D 2021
%T pCRM9 aeroelastic aircraft wing model for NASTRAN
%U https://data.4tu.nl/articles/dataset/pCRM9_aeroelastic_aircraft_wing_model_for_NASTRAN/16834387/1
%R 10.4121/16834387.v1
%K Finite Elements
%K aircraft wings
%K Nastran
%K Aeroelasticity
%X 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.<br>
%I 4TU.ResearchData