The effects of size and stacking sequence of composite laminated patch on bonded repair for cracked hole
Author:
Publisher
Springer Science and Business Media LLC
Subject
Ceramics and Composites
Link
http://link.springer.com/content/pdf/10.1007/BF00133679.pdf
Reference21 articles.
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2. Baker, A. A., Callinan, R. J., Davis, M. J., Jones, R. and Williams, J. F., ?Repair of Mirage III Aircraft Using BFRP Crack Patching Technique?, Theor. Appl. Fract. Mech. 2, 1984, 1?16.
3. Heller, M., Jones, R. and Walliams, J. F., ?Analysis of Bonded Inserts for the Repair of Fastener Holes?, Engng. Fract. Mech. 24, 1986, 523?532.
4. Heller, M., Hill, T. G., Williams, J. F. and Jones, R., ?Increasing the Fatigue Life of Cracked Fastener Holes Using Bonded Repairs?, Theor. Appl. Fract. Mech. 11, 1989, 1?8.
5. Heller, M., Jones, R. and Williams, J. F., ?Numerical Analysis of Bonded Repairs for Fastener Holes with Three-Dimensional Cracks?, Engng. Fract. Mech. 33, 1989, 81?90.
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