References
[1] Baker AA, Jones LR. Bonded Repair of Aircraft Structures : Springer Science & Business Media; 1988.
[2] Baker AA, Francis LR, Jones R. Advances in the bonded composite repair of metallic aircraft structure : Elsevier; 2003. doi:10.1016/B978-008042699-0/50000-0.
[3] Duong CN, Wang CH. Composite repair: theory and design : Elsevier; 2010. doi:10.1016/B978-008045146-6/50001-1.
[4] Baker AA, Rajic N, Davis C. Towards a practical structural health monitoring technology for patched cracks in aircraft structure.Composites Part A: Applied Science and Manufacturing 2009; 40 (9): 1340–1352. doi:https://doi.org/10.1016/j.compositesa.2008.09.015?nosfx=y
[5] Schubbe JJ, Bolstad SH, Reyes S. Fatigue crack growth behavior of aerospace and ship-grade aluminum repaired with composite patches in a corrosive environment. Composite Structures: 2016; 144: 44–56.
[6] Maldague X. Theory and practice of infrared technology for nondestructive testing . Wiley; 2001.
[7] Jones R, Baker AA, Matthews N, Champagne V. Aircraft sustainment and repair . Butterworth-Heinemann; 2017. doi:10.1016/B978-0-08-100540-8.09992-1.
[8] Martens U, Schröder K-U. Evaluation of infrared thermography methods for analysing the damage behaviour of adhesively bonded repair solutions. Composite Structures: 2020; 240. doi:https://doi.org/10.1016/j.compstruct.2020.111991
[9] Avdelidis NP, Moropoulou A, Riga ZM. The technology of composite patches and their structural reliability inspection using infrared imaging. Progress in aerospace Sciences ; 2003; 39 (4): 317–328.
[10] Paipetis AS, Grammatikos SA, Kordatos EZ, Barkoula N-M, Matikas TE. In service damage assessment of bonded composite repairs with full field thermographic techniques. In: Nondestructive Characterization for Composite Materials, Aerospace Engineering, Civil Infrastructure, and Homeland Security . San Diego: International Society for Optics and Photonics; 2011:79831U. doi:10.1117/12.880376.
[11] Moropoulou A, Avdelidis NP. Active thermography in the assessment of repaired aircraft panels. Insight 2002; 44: 145-149.
[12] Pavlopoulou S, Grammatikos SA, Kordatos EZ, Worden K, Paipetis AS, Matikas TE, Soutis C. Continuous debonding monitoring of a patch repaired helicopter stabilizer: Damage assessment and analysis.Composite Structures ; 2015; 127: 231–244.
[13] Avdelidis NP, Ibarra-Castanedo C, Maldague X, Almond DP, Moropoulou A. Thermal NDT & E of composite aircraft repairs. In:16th WCNDT 2004. Montreal: World Conference on NDT; 2004:TS4.27.3: 1-9.
[14] Grammatikos SA, Kordatos EZ, Aggelis DG, Matikas TE, Paipetis AS. Critical and subcritical damage monitoring of bonded composite repairs using innovative non-destructive techniques. In: Smart Sensor Phenomena, Technology, Networks, and Systems Integration . San Francisco: International Society for Optics and Photonics; 2012: 834611.
[15] Grammatikos SA, Kordatos EZ, Matikas TE, Paipetis AS. On the fatigue response of a bonded repaired aerospace composite using thermography. Composite Structures: 2018; 188: 461–469. doi: https://doi.org/10.1016/j.compstruct.2018.01.035.
[16] Kubin LP, Ananthakrishna G, Fressengeas C. Comment on “Portevin–Le Chatelier effect”. Physical Review E;2002; 65. doi: https://doi.org/10.1103/PhysRevE.65.053501.