References
- ABAQUS/CAE (2007), Ver 6.9 User's Manual, Hibbitt, Karlsson and Sorensen, Inc.
- Tamijani, A.Y., Mulani, S.B. and Kapania, R.K. (2017), "A multilevel framework for decomposition-based reliability shape and size optimization", Adv. Aircraft Spacecraft. Sci., 4(4), 467-486. https://doi.org/10.12989/AAS.2017.4.4.467
- Assih, J., Li, A. and Delmas, Y. (2001), "Strengthened concrete beams by gluing carbon fiber composite sheet: application of damage theory", Compos. Constr., 127, 623-628.
- Baker, A.A., Callinan, R.J., Davis, M.J., Jones, R. and Williams, J.G. (1984), "Repair of mirage III aircraft using BFRP crack patching technology", Theor. Appl. Fract. Mech., 2(1), 1-16. https://doi.org/10.1016/0167-8442(84)90035-1
- Eriksson, L., Johansson, E., Kettaneh-Wold, N., Wikstrom, C. and Wold, S. (2000), Design of Experiments: Principles and Applications, Learnways AB, Sweden.
- Frigon, N.L. and Mathews, D. (1996), Practical Guide to Experimental Design, Wiley, U.S.A.
- Goland, M. and Reissner, E. (1944), "The stresses in cemented joints", J. Appl. Mech., 11, 17-27.
- Jones, R. (1983), "Neutral axis offset effects due to crack patching", Compos. Struct., 1(2), 163-174. https://doi.org/10.1016/0263-8223(83)90010-7
- Li, A., Assih, J. and Delmas, Y. (2000), "Influence of the adhesive thickness and steel plate thickness on the behaviour of the strengthened concrete beams", J. Adhes. Sci. Technol., 14(13), 1639-1656. https://doi.org/10.1163/156856100742456
- Lubkin, J.L. (1944), "A theory of adhesive scarf joint", J. Appl. Mech., 11, 17-27.
- Elhannani, M., Madani, K., Mokhtari, M., Touzain, S., Feaugas, X. and Cohendoz, S. (2016), "A new analytical approach for optimization design of adhesively bonded single-lap joint", Struct. Eng. Mech., 59(2), 313-326. https://doi.org/10.12989/sem.2016.59.2.313
- Fioriti, M. (2014), "Adaptable conceptual aircraft design model", Adv. Aircraft Spacecraft Sci., 1(1), 43-67. https://doi.org/10.12989/aas.2014.1.1.043
- Matthews, F.L., Kilty, P.F. and Godwin, E.W. (1982), "A review of the strength of joints in fibre reinforced plastics. Part 2: Adhesively bonded joints", Compos., 13(1), 29-37. https://doi.org/10.1016/0010-4361(82)90168-9
- MODDE 5.0 (Modeling and Design) (1999), Umetrics AB, Umea, Sweden.
- Bouchiba, M.S. and Serier, B. (2016), "New optimization method of patch shape to improve the effectiveness of cracked plates repair", Struct. Eng. Mech., 58(2), 301-326. https://doi.org/10.12989/sem.2016.58.2.301
- Fekih, S.M., Albedah, A., Benyahia, F., Belhouari, M., Bouiadjra, B.B. and Miloudi, A. (2012), "Optimisation of the sizes of bonded composite repair in aircraft structures", Mater. Des., 41, 171-176. https://doi.org/10.1016/j.matdes.2012.04.025
- Tarn, J.Q. and Shek, K.L. (1991), "Analysis of cracked plates with bonded patch", Eng. Fract. Mech., 40, 1055-1065. https://doi.org/10.1016/0013-7944(91)90170-6
- Yayli, U.C., Kimet, C., Duru, A., Cetir, O., Torun, U., Aydogan, A., Padmanaban, S. and Ertas, A.H. (2017), "Design optimization of a fixed wing aircraft", Adv. Aircraft Spacecraft Sci., 4(1), 65-80. https://doi.org/10.12989/aas.2017.4.1.065
- Volkersen, O. (1938), "Die niektraftverteilung in zugbeanspruchten mit konstanten laschenquerschritten", Luftfahrtforschung, 15, 41-47.
- Cheng, X. and Wang, J. (2016), "An elastoplastic bounding surface model for the cyclic undrained behaviour of saturated soft clays", Geomech. Eng., 11(3), 325-343. https://doi.org/10.12989/gae.2016.11.3.325
- Yala, A. and Megueni, A. (2009), "Optimisation of composite patches repairs with the design of experiments method", Mater. Des., 30(1), 200-205. https://doi.org/10.1016/j.matdes.2008.04.049