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| Title: | Analysis of stagnation region heat transfer of normally impinging axisymmetric jets on solid surfaces using integral method |
| Authors: | Garg, Krati Sahu, Santosh Kumar |
| Keywords: | Boundary layers;Fighter aircraft;Heat convection;Laminar boundary layer;Nuclear energy;Nuclear engineering;Reynolds number;Axisymmetric impinging jets;Experimental test;Heat transfer characteristics;Impinging jet;Integral method;Nozzle-to-plate distance;Stagnation regions;Theoretical modeling;Heat transfer |
| Issue Date: | 2015 |
| Publisher: | American Society of Mechanical Engineers (ASME) |
| Citation: | Modak, M., Garg, K., & Sahu, S. K. (2015). Analysis of stagnation region heat transfer of normally impinging axisymmetric jets on solid surfaces using integral method. Paper presented at the International Conference on Nuclear Engineering, Proceedings, ICONE, 2015-January . |
| Abstract: | A theoretical model on heat transfer characteristics of axisymmetric impinging jets on flat solid surfaces is developed for stagnation region using energy integral method. The laminar boundary layer is divided into two regions of flow, Stagnation region and wall jet region. The present predictions were compared well with available experimental test data involving wide range coolant type, Reynolds number and nozzle to plate distance. Copyright © 2015 by JSME. |
| URI: | https://dspace.iiti.ac.in/handle/123456789/6852 |
| ISBN: | 9784888982566 |
| Type of Material: | Conference Paper |
| Appears in Collections: | Department of Mechanical Engineering |
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