Please use this identifier to cite or link to this item: https://dspace.iiti.ac.in/handle/123456789/7289
Title: Stagnation Region Heat Transfer of Axisymmetric Impinging Jets on Solid Surfaces
Authors: Garg, Krati
Sahu, Santosh Kumar
Keywords: Aspect ratio;Fighter aircraft;Heat convection;Nozzles;Prandtl number;Reynolds equation;Reynolds number;Axisymmetric impinging jets;Heat transfer characteristics;Horizontal hot surface;Impinging jet;Integral method;Nozzle-to-plate distance;Stagnation regions;Various model parameters;Heat transfer
Issue Date: 2015
Publisher: Wiley-VCH Verlag
Citation: Modak, M., Garg, K., & Sahu, S. K. (2015). Stagnation region heat transfer of axisymmetric impinging jets on solid surfaces. Chemical Engineering and Technology, 38(12), 2127-2136. doi:10.1002/ceat.201500070
Abstract: A theoretical model is proposed to evaluate the heat transfer characteristics of axisymmetric impinging fluid jets on the horizontal hot surface in the stagnation region using the energy integral method. A generalized expression involving various modeling parameters such as Nusselt number, nozzle-to-plate distance, Prandtl number, Reynolds number, and the modeling parameter k is obtained from the analysis. Present predictions are found to agree well with the test data involving a wide range of coolant type, Reynolds number, and nozzle-to-plate distance. In addition, a mechanistic correlation is suggested between the modeling parameter k and flow parameter, i.e., Reynolds number. © 2015 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim.
URI: https://doi.org/10.1002/ceat.201500070
https://dspace.iiti.ac.in/handle/123456789/7289
ISSN: 0930-7516
Type of Material: Journal Article
Appears in Collections:Department of Mechanical Engineering

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