Abstract
To accomplish the simulation of complex aircraft skin forming processes, four-node quadrilateral isoparametric element model for tool description is derived according to the stretch-forming feature of skin. In order to increase the efficiency of contact and search calculation, maximum gradient search path and precise point of intersection solving method based on imprecise intersected iterative initial value are established. Algorithm is introduced for the finite element simulation system- STRETCHFORM developed for complex skin stretch-forming processes, and the simulation for S shape skin stretch-forming processes is carried out. The good precision and stability in comparison with the results of MARC and PAM-STAMP by using exactly the same model is described. By analyzing the time consuming, it shows that contact and search algorithm based on maximum gradient search path owns higher computation efficiency than that of global search algorithm.
| Original language | English |
|---|---|
| Pages (from-to) | 308-311 |
| Number of pages | 4 |
| Journal | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| Volume | 25 |
| Issue number | 3 |
| State | Published - May 2004 |
Keywords
- Aircraft skin stretch-forming
- Contact and search
- Finite element analysis
- Four-node quadrilateral element
- Maximum gradient search method
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