Williams, Jerry G. | Search NASA

NASA NTRS1988

Multispan-Beam Shear Test For Composite Laminates

New approach for studying failure mechanism is use of multispan-beam shear test, which puts some regions of specimen in almost pure shear and enables observation of location of initial failure and way in which damage propagates. Test stopped at any time, such as when first failure event occurs, for study of phenomenon or taking photographs of failure event. Individual plies studied easily with long-distance microscope or from photographs taken during test.

Jegley, Dawn C.↗

NASA NTRS1987

The effect of resin toughness and modulus on compressive failure modes of quasi-isotropic graphite/epoxy laminates

Compressive failure mechanisms in quasi-isotropic graphite/epoxy laminates were characterized for both unnotched and notched specimens and also following damage by impact. Two types of fibers (Thornel 300 and 700) and four resin systems (Narmco 5208, American Cyanamid BP907, and Union Carbide 4901/MDA and 4901/mPDA) were studied. For all material combinations, failure of unnotched specimens was initiated by kinking of fibers in the 0-degree plies. A major difference was observed, however, in the mode of failure propagation after the 0-degree ply failure. The strength of quasi-isotropic laminates in general increased with increasing resin tensile modulus. The laminates made with Thornel 700 fibers exhibited slightly lower compressive strengths than did the laminates made with Thornel 300 fibers. The notch sensitivity as measured by the hole strength was lowest for the BP907 resin and highest for the 5208 resin. For the materials studied, however, the type of fiber had no effect on the notch sensitivity.

Hahn, H. Thomas↗