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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Main Authors: Mohd, Umair Siddiqui, Ansari, Emaad, Khan, Sher Afghan, Gulhane, Nitin Parashram, Patil, Rajesh
Format: Article
Language:English
Published: American Institute of Aeronautics and Astronautics 2020
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Online Access: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
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spelling 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
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
topic TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General)
spellingShingle 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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