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S.V. Prabhu

Researcher at Indian Institute of Technology Bombay

Publications -  182
Citations -  4757

S.V. Prabhu is an academic researcher from Indian Institute of Technology Bombay. The author has contributed to research in topics: Heat transfer & Nusselt number. The author has an hindex of 31, co-authored 168 publications receiving 3766 citations. Previous affiliations of S.V. Prabhu include Nokia & Indian Institutes of Technology.

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Experimental investigations on the effect of overlap ratio and blade edge conditions on the performance of conventional Savonius rotor

TL;DR: In this article, the torque of a conventional Savonius rotor is studied experimentally for overlap ratio from 0.10 to 0.70, blade edge condition (flat and round) and the change in Reynolds number.
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Local heat transfer distribution between smooth flat surface and impinging air jet from a circular nozzle at low Reynolds numbers

TL;DR: In this article, an experimental investigation was performed to study the effect of jet to plate spacing and low Reynolds number on the local heat transfer distribution to normally impinging submerged circular air jet on a smooth and flat surface.
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Boiling pressure drop and local heat transfer distribution of water in horizontal straight tubes at low pressure

TL;DR: In this paper, the effect of pipe diameter, heat flux and mass flux on boiling pressure drop and local heat transfer coefficient is investigated for low pressure flow boiling with water as the working medium.
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Measurement of flame emissivity of gasoline pool fires

TL;DR: In this paper, the mass burning rate of gasoline pool fires was measured using a thermography technique and the average value of the flame emissivity measured using thermography was comparable with the estimate obtained from the estimation of mass burning rates.
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Performance enhancement of a Darrieus hydrokinetic turbine with the blocking of a specific flow region for optimum use of hydropower

TL;DR: In this article, the performance of a Darrieus turbine is enhanced using a blocking plate optimally located at the upstream side of the retarding vane, which would enhance the coefficient of power of the turbine.