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Bu calismada, aluminyum-karbon elyaf sandvic levhalarin V bukme operasyonu neticesinde olusan geri esneme davranisi deneysel olarak incelenmistir. Bukme yonunun geri esneme davranisi uzerine olan etkisini incelemek amaciyla farkli bukme yonlerindeki sandvic kompozit levhalar 15°, 30°, 45°, 60°, 75° ve 90° bukme acilarinda sekillendirilmistir. Farkli bukme yonlerinde sekillendirilen sandvic kompozit levhalarda meydana gelen geri esneme degerlerinin birbirine cok yakin oldugu tespit edilmistir. Ayrica, T1 (saat yonunun tersinde) bukme yonundeki sandvic kompozit levhalarin 75° ve 90° bukme acilarindaki testlerinde aluminyum ve karbon elyaf plakalar arasinda acilmalar gorulurken, T2 (saat yonunde) bukme yonundeki sandvic kompozit levhalarin 75° ve 90° bukme acilarinda ise dis taraftaki aluminyum sac levhalarda yirtilmalar olusmustur.

Effect of bending angles and bending directions on springback in V-bending of aluminum-carbon fiber sandwich composite plates