Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD

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Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD

Researches over the recent past in the field of aerodynamic vehicles have been concerned with the problem of flow separation over its base which has lead to the formation of low pressure circulation region. This pressure is found to be noticeably lower than the free stream atmospheric pressure....

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Bibliographic Details
Main Authors:	Quadros, Jaimon Dennis, Khan, Sher Afghan, A. J., Antony, Vas, Jolene S.
Format:	Proceeding Paper
Language:	English
Published:	ISET 2016 2016
Subjects:	TL500 Aeronautics TL780 Rockets TL787 Astronautics
Online Access:	http://irep.iium.edu.my/51127/ http://irep.iium.edu.my/51127/1/51127_Experimental_and_numerical_studies.pdf

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