pCRM9 aeroelastic aircraft wing model for NASTRAN without RBE2

pCRM9 aeroelastic aircraft wing model for NASTRAN without RBE2 Based on the model published by Paul LANCELOT from Delft University of Technology, Faculty of Aerospace Engineering, Department of Aerospace Structures and Materials Lancelot, Paul (2021): pCRM9 aeroelastic aircraft wing model for NASTRAN. 4TU.ResearchData. Dataset. DOI: 10.4121/16834387.v1 Modified by: Saullo G. P. Castro removing RBE2 elements and the input related to the aeroelastic analysis. Delft University of Technology, Faculty of Aerospace Engineering, Department of Aerospace Structures and Materials Contact Information: s.g.p.castro@tudelft.nl Delft University of Technology - Faculty of Aerospace Engineering Kluyverweg 1, 2629HS Delft, The Netherlands General Introduction This is the pCRM9 aeroelastic finite element model. It is based on the University of Michigan undeflected CRM geometry: Brooks, Timothy; Kenway, Gaetan G.W.; Martins, Joaquim (2019), “uCRM: undeflected Common Research Model”, Mendeley Data, V1, DOI: 10.17632/gpk4zn73xn.1 This FEM model is tailored for optimisation and load analysis using NASTRAN. Content pCRM9_103_MAIN_FILE.bdf is the main file to run the analysis with NASTRAN SOL103, natural frequency solution. pCRM9_CONM2_MTOW.dat contains the weigth and balance informations of the model. pCRM9_mat.dat contains the material informtions of the model (in this case aluminium). pCRM9_model_2.dat contains the finite elements informations of the model (GRID, CQUAD, RBE cards etc.). pCRM9_PSHELL.dat contains the mechanical propeties for each elements of the model. pCRM9_ribs_fem.dat contains the finite elements informations relative to the ribs of the wingbox. pCRM9_FEM_model.PNG is an illustration of the structural model