R
R. M. V. G. K. Rao
Researcher at National Aerospace Laboratories
Publications - 27
Citations - 445
R. M. V. G. K. Rao is an academic researcher from National Aerospace Laboratories. The author has contributed to research in topics: Epoxy & Ultimate tensile strength. The author has an hindex of 13, co-authored 27 publications receiving 387 citations.
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Journal ArticleDOI
Low-velocity Impact Characterization of Glass, Carbon and Kevlar Composites Using Repeated Drop Tests
B. S. Sugun,R. M. V. G. K. Rao +1 more
TL;DR: In this article, repeated drop weight impact tests were carried out on advanced composites (glass, carbon, kevlar in epoxy matrix - LY 556, HT 972) using an instrumented impact test machine (DYNATUP 8250).
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Studies on Tensile and Interlaminar Shear Strength Properties of Thermally Cured and Microwave Cured Glass-Epoxy Composites
TL;DR: In this article, experimental studies were carried out on two different glass-epoxy composites (one room temperature curing epoxy-amine system and the other, an elevated temperature cured epoxyamine system) subjected to two different curing techniques (thermal and microwave), in order to investigate the effects on their thermomechanical properties.
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Characterization of Mechanical Behavior of Metallic and Non-metallic Particulate Filled Epoxy Matrix Composites
TL;DR: The results of the studies carried out on composites with three distinctly different particulate fillers, representing ductile (Cu and Al), brittle (SiC), and soft (Gr) type of materials regarding the mechanical properties, showed that the tensile and flexural strength of the particulate composites degraded with filler loading, whereas the modulus increased with the filler loading for the range of filler contents considered.
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Studies on Mechanical Behavior of Microwave and Thermally Cured Glass Fiber Reinforced Polymer Composites
TL;DR: In this article, an investigation into the mechanical behavior of microwave-cured glass-epoxy composites is carried out and the results are compared with those of thermally cured composites.
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Strength and stiffness optimization studies on honeycomb core sandwich panels
TL;DR: In this article, the optimum core to skin weight ratios for maximum stiffness and strength of the sandwich panels were experimentally found to be 2.04 and 0.96 as against the theoretical values of 2.0 and 1.0.