Compression fatigue behavior of composites in the presence of delaminationsThree different stacking sequences of a 64-ply layup were tested in an experimental investigation of the effect of idealized imbedded delaminations on the compression fatigue behavior of quasi-isotropic T300/5208 graphite-epoxy laminates. Postfailure examination of specimen cross sections revealed the absence of any fiber microbuckling, suggesting that the predominant failure mode was the propagation of imbedded delaminations in the tab region. One- and two-dimensional delaminations, respectively located across the entire width below the surface ply and buried one or four plies below the surface, were considered. A novel procedure employing minute, laser-drilled holes was successfully used in extending the application of diidobutane-enhaced radiography to buried delaminations.
Document ID
19830033344
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Authors
Ramkumar, R. L. (Northrop Corp. Aircraft Div., Hawthorne, CA, United States)