Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis

The present experimental evaluation deals with the behavior of base pressure (BP) in a suddenly expanded duct at supersonic Mach number regimes. The experiments have been conducted for two cases viz. Without and with the use of microjets or active control. The plan of experiments was planned as per...

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Main Authors:	Quadros, Jaimon Dennis, Khan, Sher Afghan, Antony, A J
Format:	Article
Language:	English
Published:	Scientific Research of the Institute of Mathematics and Computer Science 2018
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/71337/ http://irep.iium.edu.my/71337/ http://irep.iium.edu.my/71337/ http://irep.iium.edu.my/71337/1/71337_Study%20of%20base%20pressure%20behavior.pdf

id	iium-71337
recordtype	eprints
spelling	iium-713372019-07-12T07:07:27Z http://irep.iium.edu.my/71337/ Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis Quadros, Jaimon Dennis Khan, Sher Afghan Antony, A J TL Motor vehicles. Aeronautics. Astronautics The present experimental evaluation deals with the behavior of base pressure (BP) in a suddenly expanded duct at supersonic Mach number regimes. The experiments have been conducted for two cases viz. Without and with the use of microjets or active control. The plan of experiments was planned as per the Taguchi design of experiments for acquiring data in a controlled manner. An L27 orthogonal array and analysis of variance (ANOVA) has been employed to investigate the contribution (in terms of percentage) of distinct process parameters like Mach number (M), Nozzle Pressure Ratio (N), Area Ratio (A) and their interactions affecting base pressure. The correlation between these parameters affecting base pressure has been obtained using multiple linear regression analysis. It has been concluded that the Mach number and area ratio were the factors that had high statistical significance on the behavior of base pressure for both cases. The performances of the developed linear regression models have been validated for accuracy prediction by use of 15 test cases. The performance of both the base pressure models was found to be better with percentage prediction in deviation lying in the range of –12.92% to +15.88% for base pressure without control and –10.27% to +19.23% for base pressure with control. Scientific Research of the Institute of Mathematics and Computer Science 2018-12-10 Article PeerReviewed application/pdf en http://irep.iium.edu.my/71337/1/71337_Study%20of%20base%20pressure%20behavior.pdf Quadros, Jaimon Dennis and Khan, Sher Afghan and Antony, A J (2018) Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis. Journal of Applied Mathematics and Computational Mechanics, 17 (4). pp. 59-72. ISSN 2299-9965 E-ISSN 2353-0538 http://amcm.pcz.pl/?id=view&volume=17&issue=4&article=7 10.17512/jamcm.2018.4.07
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TL Motor vehicles. Aeronautics. Astronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics Quadros, Jaimon Dennis Khan, Sher Afghan Antony, A J Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
description	The present experimental evaluation deals with the behavior of base pressure (BP) in a suddenly expanded duct at supersonic Mach number regimes. The experiments have been conducted for two cases viz. Without and with the use of microjets or active control. The plan of experiments was planned as per the Taguchi design of experiments for acquiring data in a controlled manner. An L27 orthogonal array and analysis of variance (ANOVA) has been employed to investigate the contribution (in terms of percentage) of distinct process parameters like Mach number (M), Nozzle Pressure Ratio (N), Area Ratio (A) and their interactions affecting base pressure. The correlation between these parameters affecting base pressure has been obtained using multiple linear regression analysis. It has been concluded that the Mach number and area ratio were the factors that had high statistical significance on the behavior of base pressure for both cases. The performances of the developed linear regression models have been validated for accuracy prediction by use of 15 test cases. The performance of both the base pressure models was found to be better with percentage prediction in deviation lying in the range of –12.92% to +15.88% for base pressure without control and –10.27% to +19.23% for base pressure with control.
format	Article
author	Quadros, Jaimon Dennis Khan, Sher Afghan Antony, A J
author_facet	Quadros, Jaimon Dennis Khan, Sher Afghan Antony, A J
author_sort	Quadros, Jaimon Dennis
title	Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
title_short	Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
title_full	Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
title_fullStr	Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
title_full_unstemmed	Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
title_sort	study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
publisher	Scientific Research of the Institute of Mathematics and Computer Science
publishDate	2018
url	http://irep.iium.edu.my/71337/ http://irep.iium.edu.my/71337/ http://irep.iium.edu.my/71337/ http://irep.iium.edu.my/71337/1/71337_Study%20of%20base%20pressure%20behavior.pdf
first_indexed	2023-09-18T21:41:11Z
last_indexed	2023-09-18T21:41:11Z
_version_	1777413150545543168

Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis

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