Predictive modeling of suddenly expanded flow process in the Supersonic Mach number regime using response surface methodology

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Predictive modeling of suddenly expanded flow process in the Supersonic Mach number regime using response surface methodology

The present work uses design of experiments (DOE) technique along with response surface methodology to develop linear models, to establish linear input-output relationships in a suddenly expanded flow process. Mach number (M), nozzle pressure ratio (NPR), area ratio (AR) and length to diameter (L/D)...

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Bibliographic Details
Main Authors:	Quadros, Jaimon Dennis, Khan, Sher Afghan, Antony, A J
Format:	Article
Language:	English
Published:	Institute of Institutional Industrial Research 2017
Subjects:	TJ212 Control engineering
Online Access:	http://irep.iium.edu.my/61840/ http://irep.iium.edu.my/61840/1/Paper3-IJRRA-04-04-15.pdf

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