Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity
The use of air jet impingement for cooling is the most expensive task as far as the efficiency of the component is concerned not only this, but the generation of characteristic cooling over the target surface (heat sink) is of great significance in material processing firms. The conversion of the t...
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American Institute of Aeronautics and Astronautics
2020
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iium-773702020-01-28T08:09:21Z http://irep.iium.edu.my/77370/ Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity Mohd, Umair Siddiqui Ansari, Emaad Khan, Sher Afghan Gulhane, Nitin Parashram Patil, Rajesh TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General) The use of air jet impingement for cooling is the most expensive task as far as the efficiency of the component is concerned not only this, but the generation of characteristic cooling over the target surface (heat sink) is of great significance in material processing firms. The conversion of the temperature profile to a Nusselt profile is widely used when the concern of non-dimensionality comes into the picture. So, the present work reports the Nusselt profile for different impinging parameters, and the nonuniformities concerned with the profiles are evaluated. The standard deviation is the parameter used to represent the nonuniformity in the Nusselt profile for the present study. A nondimensional constant (ratio of Reynolds number and nozzle-target spacing) is defined to represent the start and end of nonuniformity in the Nusselt profile. When this constant exceeds a value of 6000, the nonuniformity in the profile ends. Also, an empirical relation representing the standard deviation is proposed in terms of the Reynolds number and nozzle-target spacing. The generation of turbulence vortices at the exit of the nozzle is responsible for the end of nonuniformity in the Nusselt profile. American Institute of Aeronautics and Astronautics 2020-01-14 Article PeerReviewed application/pdf en http://irep.iium.edu.my/77370/1/77370_Numerical%20Investigation%20of%20Non-dimensional.pdf Mohd, Umair Siddiqui and Ansari, Emaad and Khan, Sher Afghan and Gulhane, Nitin Parashram and Patil, Rajesh (2020) Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity. Journal of Thermophysics and Heat Transfer, 34 (1). pp. 1-15. ISSN 0887-8722 https://arc.aiaa.org/doi/10.2514/1.T5828 https://doi.org/10.2514/1.T5828 |
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TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General) |
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TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General) Mohd, Umair Siddiqui Ansari, Emaad Khan, Sher Afghan Gulhane, Nitin Parashram Patil, Rajesh Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity |
description |
The use of air jet impingement for cooling is the most expensive task as far as the efficiency of the component is
concerned not only this, but the generation of characteristic cooling over the target surface (heat sink) is of great significance in material processing firms. The conversion of the temperature profile to a Nusselt profile is widely used when the concern of non-dimensionality comes into the picture. So, the present work reports the Nusselt profile for different impinging parameters, and the nonuniformities concerned with the profiles are evaluated. The standard
deviation is the parameter used to represent the nonuniformity in the Nusselt profile for the present study. A
nondimensional constant (ratio of Reynolds number and nozzle-target spacing) is defined to represent the start and
end of nonuniformity in the Nusselt profile. When this constant exceeds a value of 6000, the nonuniformity in the
profile ends. Also, an empirical relation representing the standard deviation is proposed in terms of the Reynolds
number and nozzle-target spacing. The generation of turbulence vortices at the exit of the nozzle is responsible for the end of nonuniformity in the Nusselt profile. |
format |
Article |
author |
Mohd, Umair Siddiqui Ansari, Emaad Khan, Sher Afghan Gulhane, Nitin Parashram Patil, Rajesh |
author_facet |
Mohd, Umair Siddiqui Ansari, Emaad Khan, Sher Afghan Gulhane, Nitin Parashram Patil, Rajesh |
author_sort |
Mohd, Umair Siddiqui |
title |
Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity |
title_short |
Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity |
title_full |
Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity |
title_fullStr |
Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity |
title_full_unstemmed |
Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity |
title_sort |
numerical investigation of non-dimensional constant and empirical relation representing nusselt profile non-uniformity |
publisher |
American Institute of Aeronautics and Astronautics |
publishDate |
2020 |
url |
http://irep.iium.edu.my/77370/ http://irep.iium.edu.my/77370/ http://irep.iium.edu.my/77370/ http://irep.iium.edu.my/77370/1/77370_Numerical%20Investigation%20of%20Non-dimensional.pdf |
first_indexed |
2023-09-18T21:49:07Z |
last_indexed |
2023-09-18T21:49:07Z |
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