2020
DOI: 10.3390/app11010207
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Thermoelastic Investigation of Carbon-Fiber-Reinforced Composites Using a Drop-Weight Impact Test

Abstract: Composite materials are becoming more popular in technological applications due to the significant weight savings and strength offered by these materials compared to metallic materials. In many of these practical situations, the structures suffer from drop-impact loads. Materials and structures significantly change their behavior when submitted to impact loading conditions compared to quasi-static loading. The present work is devoted to investigating the thermal process in carbon-fiber-reinforced polymers (CFR… Show more

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Cited by 10 publications
(7 citation statements)
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“…Analytical results were obtained through theoretical analysis of stress profile [35][36][37][38][39] in the longitudinal direction of the sample beam similar studies were performed by Zahra et al [40][41][42][43][44]. Numerical models involved icing have been studied/reviewed by Khawaja et al and others [45][46][47][48][49][50].…”
Section: Analytical and Numerical Simulation Resultsmentioning
confidence: 99%
“…Analytical results were obtained through theoretical analysis of stress profile [35][36][37][38][39] in the longitudinal direction of the sample beam similar studies were performed by Zahra et al [40][41][42][43][44]. Numerical models involved icing have been studied/reviewed by Khawaja et al and others [45][46][47][48][49][50].…”
Section: Analytical and Numerical Simulation Resultsmentioning
confidence: 99%
“…The Finite Difference Method (FDM) is a numerical method for solving differential equations such as the two-dimensional wave [22][23][24][25][26][27], as given in Equation 1. This method approximates the differentials by discretizing the dependent variables (strain) in the independent variable domains (space and time, in this case) [27][28][29].…”
Section: Finite Difference Methods (Matlab®)mentioning
confidence: 99%
“…To bring this approximation to a three-dimensional problem, two other space coordinates 𝑗𝑗 and 𝑘𝑘 is introduced. Thus, the final FTCS FEM can be derived [32][33][34] as given in Equation 8:…”
Section: Forward-time Central-space (Ftcs) Fdmmentioning
confidence: 99%