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Ch. Nithin Chakravarthy
Researcher at CMR Institute of Technology
Publications - 23
Citations - 140
Ch. Nithin Chakravarthy is an academic researcher from CMR Institute of Technology. The author has contributed to research in topics: Indentation hardness & Flexural strength. The author has an hindex of 4, co-authored 15 publications receiving 35 citations.
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Influence of fiber loading on mechanical characterization of pineapple leaf and kenaf fibers reinforced polyester composites
TL;DR: In this article, the tensile, flexural, impact and hardness properties of kenaf fiber and pineapple leaf (PALF) reinforced with polyester composites are described for the first time.
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Effects of fiber loading on mechanical characterization of pineapple leaf and sisal fibers reinforced polyester composites for various applications
TL;DR: In this paper, the tensile, flexural, impact, and hardness properties of sisal fiber and pineapple leaf (PALF) reinforced with polyester composites are described for the first time.
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Determination of Mechanical Properties and Characterization of Alkali Treated Sugarcane Bagasse, Pine Apple Leaf and Sisal Fibers Reinforced Hybrid Polyester Composites for Various Applications
TL;DR: In this paper, the tensile, flexural, compression, impact and hardness properties of sisal fiber reinforced with polyester composites are expressed for the first time, and the experiment results revealed a consistent tendency of an increase in the above mechanical attributes to adding natural fibers/fillers.
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Dataset on tribological, characterization and thermal properties of Silicon carbide reinforced polyamide composites for industrial applications
S. Sathees Kumar,T. Vishnu Vardhan,B. Sridhar Babu,Ch. Nithin Chakravarthy,N. Prabhakar,K. Venkateswara Rao,K. Tirupathi +6 more
TL;DR: It is revealed that the addition of SIC can enhance the N6 properties and this composite can be used for high impact stress parts of gears application.
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Experimental investigation and optimization on surface parameters of ZrO2 nano particles reinforced Al-7050 metal matrix composites for aeronautical applications
TL;DR: In this paper, a composite metal framework material is created by Zirconium oxide nano powder (ZrO2) strengthening aluminum combination (Al-7050) manufactured and is set up by differing the level of weight division of the fortified particles as 5%, 10% of ZrO 2 nano powder and the rest of the aluminum compound individually.