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...
Saved in:
Main Authors: | , , |
---|---|
Other Authors: | |
Format: | Conference paper |
Published: |
2023
|
Subjects: | |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Universiti Tenaga Nasional |
id |
my.uniten.dspace-29834 |
---|---|
record_format |
dspace |
spelling |
my.uniten.dspace-298342023-12-28T16:57:50Z 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 2023-12-28T08:57:50Z 2023-12-28T08:57:50Z 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/123456789/29834 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_ |
1806423504996794368 |