APPLICATIONS
Elastoplastic analysis of aircraft fittings and tubes
A two-dimensional multi-body elastoplastic finite element analysis function was applied to a kind of necking process for connecting a high-pressure tube and a fitting of an aircraft. Residual stress due to springback and maximum separation resistance were predicted.
2D
3D
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Address
Wings Tower A1208, 12 Dongbu-ro 169beon-gil, Jinju, Gyeongsangnam-do, Republic of Korea, 52818
TEL +82-55-755-7529
FAX +82-55-761-7529
E-MAIL mfrc@afdex.com
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