Volume 14, Issue 9 (12-2014)                   Modares Mechanical Engineering 2014, 14(9): 175-182 | Back to browse issues page

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Ashenai Ghasemi F, Aligholizadeh E, Pourkamali Anaraki A. An experimental study of temperature effect on low-velocity impact response of notched aluminum plates repaired by FML composite patches. Modares Mechanical Engineering 2014; 14 (9) :175-182
URL: http://mme.modares.ac.ir/article-15-1972-en.html
Abstract:   (5472 Views)
The present research deals with the impact response of notched aluminum plates repaired by fiber metal laminate (FML) patches under various temperatures using drop weight impact test status. Some aluminum samples repaired by FML patches were prepaired to study their impact behavior and frcture mechanisms under drop weight tests at the temperature range of -20 ℃ to 60 ℃. An Energy Profiling Diagram (EPD) was used to obtain the penetration and perforation thresholds of hybrid composites. Besides, the effect of temperature on some impact characteristics such as endurance load, contact time and permanent deflection were also studied. The results showed that the amount of force for nearly all of the samples increased by increasing of the room temperature. The ability of energy absorption of the samples was also the most at the room temperature, therefore the energy thereshold of samples increases by increasing of the room temperature. Temperature variation also affects on the impact characteristics of composites patches and in some cases results in a 20 percent reduce in impact strength of the samples. It was also shown that the most value of impact parameters reaches at -20 ℃ and 60 ℃.
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Article Type: Research Article | Subject: Creep, Fatigue & Failure|Impact Mechanics|Composites
Received: 2014/01/25 | Accepted: 2014/03/14 | Published: 2014/09/24

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