Abstract The strength of randomly oriented short fiber composites has been modeled by a quasi‐isotropic laminate. Lamination theory and a failure criterion will be used to approximate the stress‐strain response of a composite as it is loaded to failure. Experimental data are presented and compared with the maximum‐strain failure criterion.
Rex J. KurigerM. Khairul AlamDavid P. Anderson
Hamid DalirSiddharth BhaganagarNicholas FrimasSeyedeh Fatemah Nabavi
Umesh GandhiSebastian GorisTim A. OsswaldYuyang Song