## Abstrad-Mode I stable crack growth results are presented under static loading through a symmetrically stiffened compact tension specimen of an aircraft grade aluminium alloy (D16AT). The results include load-deflection diagrams, J integrals, plastic zones, tunnelling (or crack front curving), e
โฆ LIBER โฆ
Finite element modelling and analysis of crack shape evolution in mode-I fatigue Middle Cracked Tension specimens
โ Scribed by R. Branco; F.V. Antunes
- Publisher
- Elsevier Science
- Year
- 2008
- Tongue
- English
- Weight
- 554 KB
- Volume
- 75
- Category
- Article
- ISSN
- 0013-7944
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