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"The production and/or worldwide consumption of chicken at an industrial or domestic level lead to a considerable quantity of chicken feather residue as a waste by-product. Chicken feathers have a possible application in preparing lightweight composites. The use of chicken feathers as a constituent to prepare hybrid composites leads to a solution for disposal of the feathers. In this study, chicken feathers were used as filler material to prepare hybrid composites. Different varieties of composites were prepared by a chicken feather hand-layup technique, and by varying the percentage weight of the chicken feathers. Specimens were prepared and tested according to ASTM standards. The 10 wt. % chicken feather-filled hybrid composites indicated the maximum tensile strength (193 MPa), flexural strength (148 MPa) and impact strength (3.65 Joules). Scanning Electron Microscopy (SEM) analysis was carried out to find the fracture and interfacial characteristics of the composites. The results indicated that, these composites can be used in domestic, automobile and structural applications which carry nominal loads."

"Penekanan setelah impak merupakan salah satu parameter penting pada komposit dengan penguat serat sebagai material struktur. Penelitian ini bertujuan untuk memperoleh nilai tekan sesudah impak dan kerusakannya pada komposit epoksi-kevlar, epoksi-gelas dan epoksi-hibrid-kevlar/gelas. Spesimen komposit difabrikasi dengan metode hand lay-up dengan variasi energi impak yang diberikan adalah 4 J, 8 J dan 15 J. Pengamatan dengan Through Transmission Ultrasonic setelah impak menunjukkan bahwa kerusakan yang terjadi adalah delaminasi. Komposit terbaik ditinjau dari nilai kuat tekan yang tinggi dan ukuran delaminasi yang paling kecil. Dapat dikatakan bahwa nilai kuat tekan tertinggi adalah epoksi-gelas yaitu sebesar 119,85 8,31 MPa.

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Compression after impact is one of important parameter of fiber reinforced composites as structural materials. This research aimed to obtain the values of compression after impact and their resulting damage on kevlar epoxy, glass epoxy, and kevlar glass epoxy hybrid composites. The composite specimens were fabricated by a hand lay up method. These materials were experienced impact energy with a variation of 4 J, 8 J, and 15 J. Observation by Through Transmission Ultrasonic showed that the type of resulting damage after impact was delamination. From this research, the highest compressive strength and the smallest delamination belongs to the glass epoxy composite, with the value of 119,85 8,31 MPa as the highest value of compression strength."