This study investigates the low-velocity impact (LVI) response of ice impactor on steel and carbon fiber rein-forced polymer (CFRP) sandwich composite. This research explores the effect of impactor's shape and length at different impact velocity by preparing customized conical and cylindrical ice impactors. Ice impactors that are frozen at -12 degrees C for 48 h are found to have the highest occurrence of partial damage, while ice impactors conditioned at -22 degrees C for 72 h experienced full damage. Although higher peak force is observed during ice-steel interaction, greater displacement and absorbed energy are evident in ice-composite impact. Results also show that full damage of ice impactor is more prominent for sandwich composite specimens, while partial damage is commonly seen in steel specimens. This is attributed to multiple hits and higher ratio of collision velocity during impact on sandwich composite. Damage type occurrences also vary depending on shape, length, and impact velocity of the ice impactors. Presence of pre-existing cracks during freezing as well as variation in stress level at the impact region influence the strength of the ice impactors. Matrix crack and facesheet dent are observed as the dominant damage mechanism in composite using X-ray micro-computed tomography. Different ice fragmentation processes are also characterized in this study.
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Arizona State Univ, Sch Engn Matter Transport & Energy, Tempe, AZ 85287 USAArizona State Univ, Sch Engn Matter Transport & Energy, Tempe, AZ 85287 USA
Liu, Yingtao
Chattopadhyay, Aditi
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Arizona State Univ, Sch Engn Matter Transport & Energy, Tempe, AZ 85287 USAArizona State Univ, Sch Engn Matter Transport & Energy, Tempe, AZ 85287 USA
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College of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, ChinaCollege of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, China
Deng, Yunfei
Liu, Bing
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College of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, ChinaCollege of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, China
Liu, Bing
Hu, Xiaoyu
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College of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, ChinaCollege of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, China
Hu, Xiaoyu
Du, Jing
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College of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, ChinaCollege of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, China
Du, Jing
Wang, Xuan
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College of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, ChinaCollege of Aeronautical Engineering, Civil Aviation University of China, Dongli District, Tianjin,300300, China