pCRM9 aeroelastic aircraft wing model for NASTRAN
DOI:10.4121/16834387.v1
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DOI: 10.4121/16834387
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
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.ResearchDataFormat
Text (.bdf .dat and .txt) and Image (.png)Associated peer-reviewed publication
pCRM9 aeroelastic model for NASTRANOrganizations
TU Delft, Faculty of Aerospace Engineering, Department of Aerospace Structures and MaterialsDATA
Files (10)
- 1,960 bytesMD5:
8c3d940841b605a91375ca6c0b3815cbREADME.txt - 1,573 bytesMD5:
5100472cdd050eae3a10567d83fbd603pCRM9_144_MAIN_FILE.bdf - 8,121 bytesMD5:
41a4c0f234d3451adfbcb032bdf0116apCRM9_aero.dat - 7,773 bytesMD5:
4fc313c4eee810a2ac7186626286bbb2pCRM9_CONM2_MTOW.dat - 233,036 bytesMD5:
203128c5030646b26ef6e7506160692epCRM9_DLM_grid.PNG - 289,499 bytesMD5:
dba8cb7c26bdbd8d61872cf85040db8epCRM9_FEM_model.PNG - 25 bytesMD5:
385878700c054e0e02edc63a99204e5apCRM9_mat.dat - 322,909 bytesMD5:
c32fd39a826c43f501f2cb910a062860pCRM9_model_2.dat - 1,075 bytesMD5:
2d47f1454c9400192913cdf0f604fd30pCRM9_PSHELL.dat - 64,371 bytesMD5:
27f4ced31536441acb99bd2fe2d0d4f8pCRM9_ribs_fem.dat -
download all files (zip)
930,342 bytes unzipped
