“…Carbon fiber-reinforced plastic/titanium alloy (CFRP/Ti) stacks are widely used as joint components with a high load-bearing capacity in the wings and fuselages of aircrafts [1][2][3][4]. CFRP/Ti stacks possess not only the advantages of CFRP [5], such as high specific strength, good vibration damping, and good fatigue resistance, but also the advantages of titanium alloys [6], such as superior strength, low density, excellent hardness, good corrosion resistance, extreme temperature resistance, etc. As a result, with the effects of improving the overall strength and achieving the lightweight demand, CFRP/Ti stacks have gradually replaced traditional alloy materials in the advanced aircraft manufacturing industry.…”