Initial gap modeling for wing assembly analysis
Author:
Funder
Russian Science Foundation
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42401-024-00302-4.pdf
Reference29 articles.
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3. Gao J, Chase KW, Magleby SP (1995) Comparison of assembly tolerance analysis by the direct linearization and modified Monte Carlo simulation methods. Proc ASME Des Eng Tech Conf 1:353–360. https://doi.org/10.1115/DETC1995-0047
4. Saadat M, Cretin L, Sim R (2009) Deformation analysis of large aerospace components during assembly. Int J Adv Manuf Technol 41:145–155. https://doi.org/10.1007/s00170-008-1464-y
5. Wang H, Si S (2014) A FEA Simulation Model for Thin-Walled C-Section Composite Beam Assembling with R-Angle Deviation. Proceedings of the ASME 2014 International Mechanical Engineering Congress and Exposition. Volume 2A: Advanced Manufacturing. https://doi.org/10.1115/IMECE2014-36956
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