Experimental Study of the Effects of Rectangular and H-Shaped Woven Nanocomposites Patch on tensile properties of Repaired AL5251 Sheets
Author:
Publisher
CMV Verlag
Link
https://mme.modares.ac.ir/article-15-53373-en.pdf
Reference26 articles.
1. Baker AA. Fatigue crack propagation studies on aluminum panels patched with boron/epoxy composite. International conference on aircraft damage assessment and repair, Melbourne, Australia; 1970.
2. Baker AA, Rose LRF, Jones R. Advances in the bonded composite repair of metallic aircraft structure. Elsevier, Amsterdam; 2002.
3. Design, analysis and performance of adhesively bonded composite patch repair of cracked aluminum aircraft panels
4. Analysis of the plastic zone size ahead of repaired cracks with bonded composite patch of metallic aircraft structures
5. Modified couple stress theory and finite strain assumption for nonlinear free vibration and bending of micro/nanolaminated composite Euler–Bernoulli beam under thermal loading
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