Publisher
Springer Nature Switzerland
Reference32 articles.
1. Okafor, A.C., Singh, N., Enemuoh, U.E., Rao, S.V.: Design, analysis and performance of adhesively bonded composite patch repair of cracked aluminum aircraft panels. Compos. Struct. 71, 258–270 (2005). https://doi.org/10.1016/j.compstruct.2005.02.023
2. Tomblin, J.S., Salah, L., Welch, J.M., Borgman, M.D.: Bonded Repair of Aircraft Composite Sandwich Structures. Report DOT/FAA/AR-03/74, 2004
3. Gul-Fang, W.: Stress analysis of plates with a circular hole reinforced by flange reinforcing member. Appl. Math. Mech. 6, 569–588 (1987). https://doi.org/10.1007/bf02017406
4. Lecture Notes in Mechanical Engineering;JG Bakuckas,2020
5. Zemlyanova, A.Y.: Reinforcement of a plate weakened by multiple holes with several patches for different types of plate-patch attachment. Math. Mech. Solids 21(3), 281–294 (2016). https://doi.org/10.1177/1081286513519812