Staff View: Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"

Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"

The first phase of this paper is aimed to develop a standard test procedure for short-duration hypersonic test facility that build at the Universiti Tenaga Nasional "UNITEN" in Malaysia. The facility has been designed, built, and commissioned for different values of diaphragm pressure rati...

Full description

Saved in:

Bibliographic Details
Main Authors:	Amir A.-F., Yusaf T., Yusoff M.Z.
Other Authors:	15750212500
Format:	Conference paper
Published:	2023
Subjects:	Gun tunnel Mach number Shock tube Shock tunnel Shock wave Calibration Diaphragms Heat flux Heat transfer Mathematical models Shock tubes Shock waves Test facilities Thermocouples Velocity measurement Gun tunnels Hypersonic test facilities Shock tunnels Hypersonic aerodynamics
Tags:	Add Tag No Tags, Be the first to tag this record!

id	my.uniten.dspace-29744
record_format	dspace
spelling	my.uniten.dspace-297442023-12-28T16:08:41Z Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification" Amir A.-F. Yusaf T. Yusoff M.Z. 15750212500 23112065900 7003976733 Gun tunnel Mach number Shock tube Shock tunnel Shock wave Calibration Diaphragms Heat flux Heat transfer Mathematical models Shock tubes Shock waves Test facilities Thermocouples Velocity measurement Gun tunnels Hypersonic test facilities Mach number Shock tunnels Hypersonic aerodynamics The first phase of this paper is aimed to develop a standard test procedure for short-duration hypersonic test facility that build at the Universiti Tenaga Nasional "UNITEN" in Malaysia. The facility has been designed, built, and commissioned for different values of diaphragm pressure ratios. A theoretical model was developed to evaluate the Mach number values as a function of diaphragm pressure ratio for different working fluids. The second phase is to run experimental tests for different operating conditions. The calculated parameters which are pressure, temperature and velocity were very comparable to the practical results. A high precision in house made thermocouple was used to measure the temperature profile during the facility operation. A numerical transient heat transfer mathematical model was developed to evaluate the heat flux from the surface temperature history. The principle of operation and the reasoning behind building such a facility are explained, and the governing equations for the shock tube are presented. Copyright � 2006 by ASME. Final 2023-12-28T08:08:41Z 2023-12-28T08:08:41Z 2006 Conference paper 2-s2.0-33845782510 https://www.scopus.com/inward/record.uri?eid=2-s2.0-33845782510&partnerID=40&md5=e65dcbf8a7dba6d5c647c9f9db958682 https://irepository.uniten.edu.my/handle/123456789/29744 2006 Scopus
institution	Universiti Tenaga Nasional
building	UNITEN Library
collection	Institutional Repository
continent	Asia
country	Malaysia
content_provider	Universiti Tenaga Nasional
content_source	UNITEN Institutional Repository
url_provider	http://dspace.uniten.edu.my/
topic	Gun tunnel Mach number Shock tube Shock tunnel Shock wave Calibration Diaphragms Heat flux Heat transfer Mathematical models Shock tubes Shock waves Test facilities Thermocouples Velocity measurement Gun tunnels Hypersonic test facilities Mach number Shock tunnels Hypersonic aerodynamics
spellingShingle	Gun tunnel Mach number Shock tube Shock tunnel Shock wave Calibration Diaphragms Heat flux Heat transfer Mathematical models Shock tubes Shock waves Test facilities Thermocouples Velocity measurement Gun tunnels Hypersonic test facilities Mach number Shock tunnels Hypersonic aerodynamics Amir A.-F. Yusaf T. Yusoff M.Z. Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"
description	The first phase of this paper is aimed to develop a standard test procedure for short-duration hypersonic test facility that build at the Universiti Tenaga Nasional "UNITEN" in Malaysia. The facility has been designed, built, and commissioned for different values of diaphragm pressure ratios. A theoretical model was developed to evaluate the Mach number values as a function of diaphragm pressure ratio for different working fluids. The second phase is to run experimental tests for different operating conditions. The calculated parameters which are pressure, temperature and velocity were very comparable to the practical results. A high precision in house made thermocouple was used to measure the temperature profile during the facility operation. A numerical transient heat transfer mathematical model was developed to evaluate the heat flux from the surface temperature history. The principle of operation and the reasoning behind building such a facility are explained, and the governing equations for the shock tube are presented. Copyright � 2006 by ASME.
author2	15750212500
author_facet	15750212500 Amir A.-F. Yusaf T. Yusoff M.Z.
format	Conference paper
author	Amir A.-F. Yusaf T. Yusoff M.Z.
author_sort	Amir A.-F.
title	Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"
title_short	Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"
title_full	Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"
title_fullStr	Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"
title_full_unstemmed	Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"
title_sort	universiti tenaga nasional short duration hypersonic test faciliy "calibration and verification"
publishDate	2023
_version_	1806427528371372032
score	13.222552

Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"

Similar Items