The pseudo-ductile response of
hybrid composites reinforced with carbon fiber veil plies is explored in this study. Laminates were fabricated by varying the number of carbon veil plies, which modified the glass fiber/carbon fiber veil thickness ratio to achieve stable pseudo-ductile behavior. Stress–strain curves were experimentally obtained to assess the influence of this thickness ratio on curve flattening. The results demonstrated pseudo-ductile behavior characterized by gradual, progressive failure, achieving a pseudo-ductile strain of up to 7.096%. An improvement of up to 450% in pseudo-ductility was achieved compared to values reported in the literature, highlighting the potential of carbon fiber veil as a low-cost reinforcement for developing pseudo-ductile composites using low-performance materials.