Interlaminar fracture toughness and delamination fatigue crack growth behavior were investigated for carbon fiber (CF)/epoxy laminates with the self-same epoxy interleaf. The matrix epoxy with a thickness of 50 lm was chosen as the interleaf material in order to clarify the effect of resin-rich laye
β¦ LIBER β¦
Mode I delamination fatigue properties of interlayer-toughened CF/epoxy laminates
β Scribed by Masaki Hojo; Satoshi Matsuda; Mototsugu Tanaka; Shojiro Ochiai; Atsushi Murakami
- Book ID
- 108104031
- Publisher
- Elsevier Science
- Year
- 2006
- Tongue
- English
- Weight
- 974 KB
- Volume
- 66
- Category
- Article
- ISSN
- 0266-3538
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Modes I and II interlaminar fracture tou
β
Masaki Hojo; Tadashi Ando; Mototsugu Tanaka; Taiji Adachi; Shojiro Ochiai; Yoshi
π
Article
π
2006
π
Elsevier Science
π
English
β 721 KB
Rate Effects on Mode-I Delamination Toug
β
Xiang-Fa Wu; Yuris A. Dzenis
π
Article
π
2001
π
Springer Netherlands
π
English
β 162 KB
Mode I delamination of angle-ply epoxy/g
β
M.N. Charalambides; J.G. Williams
π
Article
π
1994
π
Elsevier Science
π
English
β 823 KB
Effects of Stitching on Delamination of
β
Walid Trabelsi; Laurent Michel; Renaud Othomene
π
Article
π
2010
π
Springer Netherlands
π
English
β 972 KB
Fatigue delamination, initiation, and gr
β
Antonio ArgΓΌelles; Jaime ViΓ±a; Alfonso F. Canteli; Jorge Bonhomme
π
Article
π
2009
π
Society for Plastic Engineers
π
English
β 406 KB
## Abstract In this article, interlaminar crack initiation and propagation under mode I and II dynamic loading of an epoxy matrix reinforced with unidirectional carbon fibers were evaluated. Delamination in mode I was carried out employing the DCB test (Double Cantilever Beam). In mode II, the ENF
Cryogenic Interlaminar Fracture Properti
β
Masaya Miura, Yasuhide Shindo, Tomo Takeda, Fumio Narita
π
Article
π
2012
π
Springer Netherlands
π
English
β 751 KB