|کد مقاله||کد نشریه||سال انتشار||مقاله انگلیسی||ترجمه فارسی||نسخه تمام متن|
|5015401||1464040||2018||9 صفحه PDF||سفارش دهید||دانلود رایگان|
- Impact behavior of scarf-repaired laminates was investigated experimentally and numerically.
- The adhesive can efficiently protect the parent from impact damage.
- Scarf angle, adhesive thickness and patch off-axis angle affect impact properties.
- Ranges of above parameters were recommended for less impact damage.
Low-velocity impact performance of scarf-repaired composite laminates was investigated by experimental and numerical methods. The numerical model was built using continuum damage mechanics and cohesive elements were used in all the interfaces of the adherends (i.e. the patch and the parent). The model was verified to be efficient. Based on it, damage profiles and damage mechanism were studied, and the effects of the scarf angle, the adhesive thickness and the patch off-axis angles were analyzed. Results show that the patch damage occurs in its center region through the thickness, while the damages in the parent and adhesive mainly occur around the back face. Damage area of the patch is obviously more serious than that of the parent, and the adhesive can protect the parent to some degree. The scarf angle, the adhesive thickness and the patch off-axis angles have effects on the impact properties. The scarf angles ranging from 7Â° to 8Â°, the adhesive thicknesses of 0.15â¯mm, the patch off-axis angles ranging from 135Â° to 160Â° are recommended for better impact performances.
Journal: International Journal of Impact Engineering - Volume 111, January 2018, Pages 85-93