Aerospace-grade aluminum alloys, such as 2195 (Al-Cu-Li) and 2219 (Al-Cu), are pivotal in the fabrication of lightweight, high-strength components for aerospace applications, including rocket fuel tanks, aircraft envelopes, and structural panels. These alloys are prized for their exceptional mechanical properties, including high specific strength, excellent corrosion resistance, and good weldability. However, the manufacturing processes, particularly spinning, introduce complex residual stress distributions that can significantly affect the dimensional stability, mechanical performance, and long-term reliability of these components. Spinning, a metal-forming process involving the rotation of a workpiece against a tool to shape it, induces significant plastic deformation, leading to residual stresses that evolve during subsequent aging treatments. This article explores the residual stress distribution and aging stability evolution in 2195 and Read more