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Key technology research and system development of complex aircraft skin stretch-forming simulation

  • Di Bai*
  • , Xian Bin Zhou
  • , Dong Sheng Li
  • , Yi Cheng Liu
  • *此作品的通讯作者
  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

To pre-estimate the formability of complex aircraft skin parts and simulate the whole deformation processes, a finite element simulation system-STRETCHFORM is developed to assist the manufacture according to the stretch-forming feature of skin parts. The system is composed of three function modules-pre-processing, solving and post-processing, and key techniques including motion of mechanism, static implicit algorithm, contact and search algorithm as well as evaluation criterion of forming quality are analyzed and accomplished. Simulations of stretch-forming process for S shape skin and air inlet part are carried out, demonstrating the good precision and stability in comparison with the results of MARC, PAM-STAMP and experiment.

源语言英语
页(从-至)606-610
页数5
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
25
6
出版状态已出版 - 11月 2004

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