3347
博碩士論文
Engineering Science and Mechanics
The damage development and strength ofply-level scaled carbon/epoxy compositelaminates having stacking sequence of[+Tn/-Tn/902n]s where constraint ply angle, T,was 0, 15, 30, 45, 60, and 75 degrees, andsize was scaled as n=1,2,3, and 4, is reportedin Part I. X-radiography was used to monitordamage developments. First-ply failure stress,and tensile strength were recorded. First-plyfailure of the midplane 90 deg. plies dependedon the stiffness of constraint plies, and size. All24 cases were predic...