High speed flow characteristics in gun tunnel

Research in supersonic remains a concern in many applications and maybe conducted using ground-based experimental facilities, computational fluid dynamics (CFD) or actual flight tests using rocket powered flight vehicles. An experimental study was performed to establish investigative work on the tra...

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Main Authors: Ahmed D.I., Yusoff M.Z., Amir A.-F., Kasolang S.
Other Authors: 35753100700
Format: Conference paper
Published: Elsevier Ltd 2023
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spelling my.uniten.dspace-294762023-12-28T14:30:10Z High speed flow characteristics in gun tunnel Ahmed D.I. Yusoff M.Z. Amir A.-F. Kasolang S. 35753100700 7003976733 15750212500 10938903300 Gun Tunnel High speed flow Peak pressure Shock strength Shock wave speed Research in supersonic remains a concern in many applications and maybe conducted using ground-based experimental facilities, computational fluid dynamics (CFD) or actual flight tests using rocket powered flight vehicles. An experimental study was performed to establish investigative work on the transient flow behaviour in short duration high speed flow gun tunnel test facility available in Universiti Tenaga Nasional (UNITEN). Physical descriptions of the facility along with the principle of operation have been described. The pressure history of flow process was captured using a fast response pressure transducers at three stations located at the end of the facility. Experimental measurements of shock strength, peak pressure and shock wave speed change of Air-Air as a driver/driven gas were presented and compared with another set of experimental measurements using a gas combination of Helium-Air. In this study, deployment of two pressure transducers technique has made measurement of the shock wave speed easy. It was also observed that the existence of the piston has a very significant influence on the moving shock wave and peak pressure value obtained. The results provide a very good estimate of the parameters being investigated after diaphragm rupture and also offer better understanding of the parameters affecting the performance of the facility. � 2012 The Authors. Final 2023-12-28T06:30:10Z 2023-12-28T06:30:10Z 2012 Conference paper 10.1016/j.proeng.2012.07.384 2-s2.0-84901028844 https://www.scopus.com/inward/record.uri?eid=2-s2.0-84901028844&doi=10.1016%2fj.proeng.2012.07.384&partnerID=40&md5=a67aed65b45eec4d8881def5803a325f https://irepository.uniten.edu.my/handle/123456789/29476 41 1787 1793 All Open Access; Gold Open Access Elsevier Ltd 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
High speed flow
Peak pressure
Shock strength
Shock wave speed
spellingShingle Gun Tunnel
High speed flow
Peak pressure
Shock strength
Shock wave speed
Ahmed D.I.
Yusoff M.Z.
Amir A.-F.
Kasolang S.
High speed flow characteristics in gun tunnel
description Research in supersonic remains a concern in many applications and maybe conducted using ground-based experimental facilities, computational fluid dynamics (CFD) or actual flight tests using rocket powered flight vehicles. An experimental study was performed to establish investigative work on the transient flow behaviour in short duration high speed flow gun tunnel test facility available in Universiti Tenaga Nasional (UNITEN). Physical descriptions of the facility along with the principle of operation have been described. The pressure history of flow process was captured using a fast response pressure transducers at three stations located at the end of the facility. Experimental measurements of shock strength, peak pressure and shock wave speed change of Air-Air as a driver/driven gas were presented and compared with another set of experimental measurements using a gas combination of Helium-Air. In this study, deployment of two pressure transducers technique has made measurement of the shock wave speed easy. It was also observed that the existence of the piston has a very significant influence on the moving shock wave and peak pressure value obtained. The results provide a very good estimate of the parameters being investigated after diaphragm rupture and also offer better understanding of the parameters affecting the performance of the facility. � 2012 The Authors.
author2 35753100700
author_facet 35753100700
Ahmed D.I.
Yusoff M.Z.
Amir A.-F.
Kasolang S.
format Conference paper
author Ahmed D.I.
Yusoff M.Z.
Amir A.-F.
Kasolang S.
author_sort Ahmed D.I.
title High speed flow characteristics in gun tunnel
title_short High speed flow characteristics in gun tunnel
title_full High speed flow characteristics in gun tunnel
title_fullStr High speed flow characteristics in gun tunnel
title_full_unstemmed High speed flow characteristics in gun tunnel
title_sort high speed flow characteristics in gun tunnel
publisher Elsevier Ltd
publishDate 2023
_version_ 1806428036626644992
score 13.214268