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The composite materials are more demand in industrial and aerospace sectors having very good passive damping in order to mitigate the amplitude of vibrations caused during dynamic service conditions. Hybrid composites are widely used in the structural applications like aircraft, automotive, marine, and machine tool structures owing to their excellent strength to weight ratio, cost effectiveness and nowadays they replace metallic materials predominantly. The recent fabrication of structures in hybrid composites contains reinforcing organic and inorganic nature. The wastage particles such as RHA and fly ash are interlaced in two mutually orthogonal directions to one another which promote excellent integrity and conformability and balanced mechanical properties within the fabric plane. Because of these advantages hybrid composites become popular in all such mentioned structural applications. The investigation mainly focus on fatigue life influenced by organic and inorganic particles with different weight fraction measured at different stress levels over a wide range spectrum of three different materials are evaluated and compared. The mechanical properties such as fatique strength, hardness and compressive strength were studied for all specimens. The micro/macro cracks and fracture surface are revealed under the scanning electron microscope (SEM) analysis. Optical microscope (OM) analysis is used to find out the difference at different stress level conditions to determine the safe stress level.

EXPERIMENTAL INVESTIGATION OF MECHANICAL PROPERTIES OF RICE HUSK ASH , FLY ASH REINFORCED WITH Al 356 -HYBRID COMPOSITES