## 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
MODE I AND MIXED-MODE STABLE CRACK EXTENSIONS THROUGH STIFFENED THREE-POINT BEND SPECIMENS
โ Scribed by A.-H. I. Mourad; S. K. Maiti
- Book ID
- 109013653
- Publisher
- John Wiley and Sons
- Year
- 1995
- Tongue
- English
- Weight
- 832 KB
- Volume
- 18
- Category
- Article
- ISSN
- 8756-758X
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Using specimens of western hemlock with various depths, double cantilever beam and three-point bend end-notched flexure tests were conducted to obtain the mode I and mode II fracture toughness. To correct the deflection caused by shearing and crack tip deformation, four conventional data reduction m