This paper presents an automated approach to extract strains of aircraft structural models from widely used CAD and FE environments. The developed approach has been implemented as an integrated tool in widely used CATIA V5 and Abaqus environment. The integrated tool is a quick inexpensive and effecive technique for predicting structural strains.
| Attachment | Size |
|---|---|
| Udali_Infosys_final_2242012.pdf | 536.03 KB |