Author:
Okafor A. Chukwujekwu,Singh Navdeep,Enemuoh U.E.,Rao S.V.
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference12 articles.
1. Baker AA. Fatigue crack propagation studies on aluminum panels patched with boron/epoxy composites. In: International conference on aircraft damage assessment and repair, Melbourne, August 1991. p. 209–15.
2. Analysis of cracked aluminum plates repaired with bonded composite patches;Sun;AIAA J,1996
3. Modeling of patch repair to a thin cracked sheet;Umamaheswar;Eng Fract Mech,1999
4. Belason EB, Rutherford P, Miller M. Evaluation of bonded boron/epoxy doublers for commercial aircraft aluminum structures. In: Harris CE, editor. FAA/NASA Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, NASA CP 3274, September 1994.
5. Strength prediction of patch repaired CFRP laminates loaded in compression;Hu;Compos Sci Technol,2000
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