ASTM STP23702S PDF
Application of the Hybrid Finite Element Method to Aircraft Repairs
Название (английский):
ASTM STP23702S
Application of the Hybrid Finite Element Method to Aircraft Repairs
- Статус документа:
- D
- Формат:
- Электронный (PDF)
- SKU:
- ASTM STP23702S
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Abstract
A hybrid finite element approach is presented for the analysis of cracked panels with riveted doublers in airframe structures. The method uses the super element developed by Tong to model the cracked panel with rivet holes, springs to model...
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