Practical Applications of Improvements in Fml Crack Bridging Theory-Reference-Cited by-同舟云学术

Practical Applications of Improvements in Fml Crack Bridging Theory

Published:2009 Issue: Volume: Page:539-558
ISSN:
Container-title:ICAF 2009, Bridging the Gap between Theory and Operational Practice
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Author:

Wilson Greg,Alderliesten René,Rodi Riccardo,Lemmen H. J. K.

Publisher

Springer Netherlands

Link

http://link.springer.com/content/pdf/10.1007/978-90-481-2746-7_31.pdf

Reference12 articles.

1. Vermeeren, C. (2002), Around Glare: a new aircraft material in context, Kluwer Academic Publishers.

2. Wu, H. F., Bucci, R. J., Wygonik, R. H., and Rice, R. C. (1993). AIAA J. of Aircraft, Vol. 30, no. 2, pp. 275–282.

3. Roebroeks, G. H. J. J., Hooijmeijer, P. A., Kroon, E. J., and Heinimann, M. B., (2007). In: First International Conference on Damage Tolerance of Aircraft Structures, Benedictus, R., Schijve, J., Alderliesten, R. C., and Homan, J. J. (Eds.), Delft, The Netherlands.

4. Alderliesten, R. C. (2007), Intl. J. of Fatigue, Vol. 29, pp. 628–646.

5. Wu, X. R. and Guo, Y. J. (2002), Fatigue Fract. Eng. Mat. Struct., Vol. 25, pp. 417–432.

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