S
Sher Afghan Khan
Researcher at International Islamic University Malaysia
Publications - 270
Citations - 2513
Sher Afghan Khan is an academic researcher from International Islamic University Malaysia. The author has contributed to research in topics: Mach number & Nozzle. The author has an hindex of 18, co-authored 248 publications receiving 1782 citations. Previous affiliations of Sher Afghan Khan include International University, Cambodia & P A College of Engineering.
Papers
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Active Control of Suddenly Expanded Flows from Overexpanded Nozzles
TL;DR: In this paper, an experimental investigation was carried out to study the effectiveness of micro-jets to control base pressure in suddenly-expanded axi-symmetric ducts, and it was found that the microjets can serve as active controllers for increasing or decreasing base pressure.
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Response surface analysis, clustering, and random forest regression of pressure in suddenly expanded high-speed aerodynamic flows
Asif Afzal,Abdul Aabid,Ambareen Khan,Sher Afghan Khan,Upendra Rajak,Tikendra Nath Verma,Rajesh Kumar +6 more
TL;DR: In this article, the authors performed an experimental analysis of base pressure in suddenly expanded compressible flow from nozzles at different Mach numbers and found that microjets are efficient when the flow is under the influence of a favorable pressure gradient.
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Nusselt number analysis from a battery pack cooled by different fluids and multiple back-propagation modelling using feed-forward networks
Imran Mokashi,Imran Mokashi,Asif Afzal,Sher Afghan Khan,Nur Azam Abdullah,Muhammad Hanafi Azami,Ravindra Jilte,Olusegun David Samuel +7 more
TL;DR: In this article, an analysis of average Nusselt number (Nuavg), which indicates the heat removal from the battery pack cooled by flowing fluid is carried out considering coupled heat transfer condition at the pack and coolant interface.
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Control of Suddenly Expanded Flows with Micro-Jets
TL;DR: In this paper, the results of an experimental investigation carried out to control the base pressure in a suddenly expanded axi-symmetric passage are presented in order to identify the L/D which will result in maximum increase/decrease of base pressure.
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Control of suddenly expanded flow
TL;DR: In this paper, the effectiveness of micro jets under the influence of Over, Under, and Correct expansion to control the base pressure in suddenly expanded axi-symmetric ducts was investigated.