Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers

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Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers

In this investigation the flow field has been computed by the numerical approach using Computational Fluid Dynamics (CFD) Analysis to investigate the efficacy of the supersonic Mach numbers due to the flow from supersonic nozzle exhausted in a larger circular duct and the corresponding thrust force...

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Bibliographic Details
Main Authors:	Pathan, Khizer Ahmed, Dabeer, P. S., Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	Elsevier 2018
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/66581/ http://irep.iium.edu.my/66581/1/66581_Optimization%20of%20area%20ratio%20and%20thrust.pdf http://irep.iium.edu.my/66581/7/66581%20Optimization%20of%20area%20ratio%20and%20thrust%20in%20suddenly%20expanded%20flow%20at%20supersonic%20SCOPUS.pdf

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