Simple and Generalized Residual Strength Model for Damaged CompositesSource: Journal of Aerospace Engineering:;1988:;Volume ( 001 ):;issue: 003Author:C. S. Chu
DOI: 10.1061/(ASCE)0893-1321(1988)1:3(131)Publisher: American Society of Civil Engineers
Abstract: A simple and generalized static residual' strength model was formulated on the basis of equivalent damage size concept and stress fracture criterion. The model is semiempirical in nature and requires two data points, i.e., one test for the undamaged case and another with a damaged specimen. Good correlations were obtained with either impact‐damaged or simulated delamination tests. Theoretically speaking, this model can be applied to any type of damage.
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| contributor author | C. S. Chu | |
| date accessioned | 2017-05-08T21:15:31Z | |
| date available | 2017-05-08T21:15:31Z | |
| date copyright | July 1988 | |
| date issued | 1988 | |
| identifier other | %28asce%290893-1321%281988%291%3A3%28131%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44635 | |
| description abstract | A simple and generalized static residual' strength model was formulated on the basis of equivalent damage size concept and stress fracture criterion. The model is semiempirical in nature and requires two data points, i.e., one test for the undamaged case and another with a damaged specimen. Good correlations were obtained with either impact‐damaged or simulated delamination tests. Theoretically speaking, this model can be applied to any type of damage. | |
| publisher | American Society of Civil Engineers | |
| title | Simple and Generalized Residual Strength Model for Damaged Composites | |
| type | Journal Paper | |
| journal volume | 1 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(1988)1:3(131) | |
| tree | Journal of Aerospace Engineering:;1988:;Volume ( 001 ):;issue: 003 | |
| contenttype | Fulltext |