Aerospace
Journal Article

Methodology for Solving Contact Problem during Riveting Process

SAE International Journal of Aerospace

2011-01-2582

10/18/2011

Event
Aerospace Technology Conference and Exposition
Authors
Sergey Lupuleac St. Petersburg Politechnic Univ.
Margarita Petukhova St Petersburg Politechnic Univ
Yulia Shinder St Petersburg Politechnic Univ
Bertrand Bretagnol Airbus
Abstract
Content
The paper describes the methodology of contact problem solving that is used in specialized software code aimed at simulation of aircraft assembly process. For considered class of problems it is possible to radically reduce the number of unknowns without loss of accuracy.
The results of validation of developed code against physical experiments and commercial FEM codes are also given.
Meta Tags
Topics
Assembling
Finite element analysis
Aircraft
Fastening
Simulation and modeling
Computer software and hardware
Affiliated or Co-Author
St. Petersburg Politechnic Univ.
St Petersburg Politechnic Univ
Airbus
Details
DOI
https://doi.org/10.4271/2011-01-2582
Pages
6
Citation
Lupuleac, S., Petukhova, M., Shinder, Y., and Bretagnol, B., "Methodology for Solving Contact Problem during Riveting Process," SAE Int. J. Aerosp. 4(2):952-957, 2011, https://doi.org/10.4271/2011-01-2582.
Additional Details
Publisher
SAE International
Published
Oct 18, 2011
Product Code
2011-01-2582
Content Type
Journal Article
Language
English

Journal

SAE International Journal of Aerospace
SAE International Journal of Aerospace Image
Volume 4, Issue 2