Finite element model updating on structural components of simplified model of aircraft pylon
Assumptions and simplifications in finite element (FE) modelling for structural vibration analysis contribute to discrepancies in numerical results. This paper presents FE model updating on components of a simplified model of an aircraft pylon. The components are tested under free-free boundary cond...
| الحاوية / القاعدة: | AIP Conference Proceedings |
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| المؤلف الرئيسي: | |
| التنسيق: | Conference paper |
| اللغة: | English |
| منشور في: |
American Institute of Physics Inc.
2022
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| الوصول للمادة أونلاين: | https://www.scopus.com/inward/record.uri?eid=2-s2.0-85141852671&doi=10.1063%2f5.0103288&partnerID=40&md5=135904ad92f10dcdecd0ab2be2e32ba5 |