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This paper has presented an experimental study of quasi-static compressive and tensile  loading of cutout hole on multi-layer of Kevlar-29/epoxy-Al 2 O 3 laminated composite. The  experimental procedure has been developed to study the performance of (50%, 55% and 60%)  volume fraction (vf) and (0 o /90 o and +45 o /-45 o ) fiber orientation angle effects of these composites  under quasi-static compressive and tensile load using a servo-hydraulic testing machine. It was  concluded that the maximum load bearing capacity increases as volume fraction increases in  tensile test. While, the maximum load bearing capacity increases with the decrease of volume  fraction in compression test. Hence, from the results obtained it can considered the 55% volume  fraction of composite panels is a good value for tensile and compression applications.

An Experimental Study of Circular Cutout Hole Effect of Kevlar/epoxy-Al2O3 Composite under Subjected to Quasi-Static Compressive and Tensile Loading