Experimental study of suddenly expanded flow from correctly expanded nozzles

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Experimental study of suddenly expanded flow from correctly expanded nozzles

This paper presents the results of the experimental investigation conducted at supersonic Mach numbers through converging–diverging nozzles. The experiments were conducted for correctly expanded cases and, for length-to-diameter ratio of 10 to 1. The area ratios were 1.6, 1.8, 2.2, and 6.25. The r...

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Bibliographic Details
Main Authors:	Khan, Sher Afghan, G M, Fharukh Ahmed
Format:	Proceeding Paper
Language:	English
Published:	Department of Mechanical Engineering Saveetha School of Engineering Saveetha University 2016
Subjects:	TL780 Rockets TL787 Astronautics
Online Access:	http://irep.iium.edu.my/51129/ http://irep.iium.edu.my/51129/4/51129.pdf

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