When these data are applied to the formula derived by M. A. Schroedl and C. W. Smith, the stress intensity factor K, can be calculated. Comparing this computed K, with that given by theoretical formula, we have found the error to be within t 5.20%. It is believed that the result of this test has met
The calculation of the strain energy release rates and the stress intensity factors for several crack conditions
β Scribed by Wei-Yang Huang
- Publisher
- Elsevier Science
- Year
- 1982
- Tongue
- English
- Weight
- 71 KB
- Volume
- 16
- Category
- Article
- ISSN
- 0013-7944
No coin nor oath required. For personal study only.
β¦ Synopsis
Chinese abstracts 133 The experimental results show that (I) X, of two thin sheet aluminum alloys are valid; they_ are I?, = 201.39 kg/mm"* and l?,, = 208.31 kg/mm"2 of Lyl22c2(1), K, =226.18kg/mm"2 and K,,= 234.55 kg/mm3" of Lc4 -cs; (2) the R-curves of the four thin sheet aluminum alloys are independent of the initial crack length of specimen; (3) for different initial crack lengths the crack growth Aa is not a constant.
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