International audienceThe excellent combination of light-weight and good mechanical propertiesmakes titanium alloys attractive for compressor section components in gasturbine engines (temperature between 250 and 600 C). However, above 600 C,the formation of an unprotective oxide layer facilitates the oxygen diffusion into thealloy. In this experimental study, pure titanium was treated with mechanical surfacetreatment to promote better protection against oxidation at high temperature. Shotpeenedand laser-shock peened specimens were compared to untreated samples interms of oxidation behavior at high temperature. We used thermal gravimetricanalysis to oxidize the samples at 700 C for 100 h. Subsequently, XRD, opticalmicroscopy, SEM/EDS, NRA, micro-Raman spectroscopy, and micro-hardnesswere used to characterize the oxide scale and the alpha-case layer formed during thehigh-temperature exposure. The shot-peened samples oxidized less (-45%) than theuntreated and laser-shock peened samples. This behavior was attributed to theformation of a continuous nitride layer between oxide and meta