Simulation of two-way interaction between sealant and structural parts as applied to large-scale aircraft assembly
Author:
Funder
Russian Science Foundation
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s00170-024-13535-6.pdf
Reference47 articles.
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2. Baklanov S, Stefanova M, Lupuleac S (2020) Newton projection method as applied to assembly simulation. Optim Methods Softw 37(2):577–604. https://doi.org/10.1080/10556788.2020.1818079
3. Bartczak B, Mucha J, Trzepieciński T (2013) Stress distribution in adhesively-bonded joints and the loading capacity of hybrid joints of car body steels for the automotive industry. Int J Adhes Adhes 45:42–52. https://doi.org/10.1016/j.ijadhadh.2013.03.012
4. Bird R, Armstrong R, Hassager O (1987) Dynamics of polymeric liquids, vol. 1 : Fluid mechanics. Wiley, New York
5. Burka P, Liu X, Thompson M et al (2013) Modelling of adhesive bonding for aircraft structures applying the insertion squeeze flow method. Compos B 50:247–252. https://doi.org/10.1016/j.compositesb.2013.02.019
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1. Modeling and analysis of hybrid bonded-bolted joining in large-scale aircraft assembly;2024-08-26
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