The authors have earlier proposed a small cylindrical circumferentially notched and fatigue cracked specimen for estimating K,, Finite element studies carried out are discussed with specific attention to the comparison between K,( thus obtained to that obtained experimentally. The size of the plasti
β¦ LIBER β¦
Fracture toughness and ndt requirements for aircraft design
β Scribed by P.F. Packman
- Publisher
- Elsevier Science
- Year
- 1973
- Weight
- 935 KB
- Volume
- 6
- Category
- Article
- ISSN
- 0029-1021
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