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Showing items 1-4 of 4 (1 Page(s) Totally)
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| 臺大學術典藏 |
2019-12-10T03:44:36Z |
A methodology for fatigue crack growth and residual strength prediction with applications to aircraft fuselages
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Chen, C.-S.; Wawrzynek, P.A.; Ingraffea, A.R.; CHUIN-SHAN CHEN |
| 臺大學術典藏 |
2019-12-10T03:44:34Z |
Prediction of residual strength and curvilinear crack growth in aircraft fuselages
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Chen, C.-S.; Wawrzynek, P.A.; Ingraffea, A.R.; CHUIN-SHAN CHEN |
| 臺大學術典藏 |
2019-12-10T03:44:34Z |
Residual strength prediction of aircraft fuselages using crack-tip opening angle criterion
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Chen, C.-S.; Wawrzynek, P.A.; Ingraffea, A.R.; CHUIN-SHAN CHEN |
| 國立臺灣大學 |
2002 |
Prediction of Residual Strength and Curvilinear Crack Growth in Aircraft Fuselage
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Chen, C.-S.; Wawrzynek, P. A.; Ingraffea, A. R. |
Showing items 1-4 of 4 (1 Page(s) Totally)
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