Numerical simulations of transient flows in shock tube and validations with experimental measurements

This paper describes the numerical simulations of transient flows in shock tube which involves multiple reflections of shockwaves, contact surface and expansion waves and their interactions. The numerical formulations solve the fully compressible Reynolds Averaged Navicr Stokes (RANS) equations set...

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Main Authors: Yusoff M.Z., Al-Falahi A., Shuaib N.H., Yusaf T.
Other Authors: 7003976733
Format: Conference paper
Published: EUROSIS 2023
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spelling my.uniten.dspace-297042023-12-28T15:41:43Z Numerical simulations of transient flows in shock tube and validations with experimental measurements Yusoff M.Z. Al-Falahi A. Shuaib N.H. Yusaf T. 7003976733 15750212500 13907934500 23112065900 Shocktube Shockwave Transient high speed flows Computer simulation Finite volume method Numerical methods Numerical models Shock waves Transition flow Different operating conditions Experimental test High speed flows Multiple reflections Numerical formulation Numerical results Reflected shock waves Reynolds averaged Shock tubes This paper describes the numerical simulations of transient flows in shock tube which involves multiple reflections of shockwaves, contact surface and expansion waves and their interactions. The numerical formulations solve the fully compressible Reynolds Averaged Navicr Stokes (RANS) equations set using finite volume method. The numerical results are validated against analytical solutions and experimental measurements in the high speed flow test facility available at the Universiti Tenaga Nasional (UNITEN), Malaysia. Experimental tests for different operating conditions have been performed. High precision pressure transducers were used to measure the pressure history at two different locations within the shock tube. Experimental results were compared with the numerical results and good agreements were obtained. The numerical simulations also revealed that the flow tend to be very unstable in the region close to the diaphragm after the reflected shock wave interacts with the contact surface. � 2008 EUROSIS-ETI. Final 2023-12-28T07:41:43Z 2023-12-28T07:41:43Z 2008 Conference paper 2-s2.0-84899033282 https://www.scopus.com/inward/record.uri?eid=2-s2.0-84899033282&partnerID=40&md5=2a6bb958417bcbb989d5eaf311da5bc8 https://irepository.uniten.edu.my/handle/123456789/29704 5 11 EUROSIS 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 Shocktube
Shockwave
Transient high speed flows
Computer simulation
Finite volume method
Numerical methods
Numerical models
Shock waves
Transition flow
Different operating conditions
Experimental test
High speed flows
Multiple reflections
Numerical formulation
Numerical results
Reflected shock waves
Reynolds averaged
Shock tubes
spellingShingle Shocktube
Shockwave
Transient high speed flows
Computer simulation
Finite volume method
Numerical methods
Numerical models
Shock waves
Transition flow
Different operating conditions
Experimental test
High speed flows
Multiple reflections
Numerical formulation
Numerical results
Reflected shock waves
Reynolds averaged
Shock tubes
Yusoff M.Z.
Al-Falahi A.
Shuaib N.H.
Yusaf T.
Numerical simulations of transient flows in shock tube and validations with experimental measurements
description This paper describes the numerical simulations of transient flows in shock tube which involves multiple reflections of shockwaves, contact surface and expansion waves and their interactions. The numerical formulations solve the fully compressible Reynolds Averaged Navicr Stokes (RANS) equations set using finite volume method. The numerical results are validated against analytical solutions and experimental measurements in the high speed flow test facility available at the Universiti Tenaga Nasional (UNITEN), Malaysia. Experimental tests for different operating conditions have been performed. High precision pressure transducers were used to measure the pressure history at two different locations within the shock tube. Experimental results were compared with the numerical results and good agreements were obtained. The numerical simulations also revealed that the flow tend to be very unstable in the region close to the diaphragm after the reflected shock wave interacts with the contact surface. � 2008 EUROSIS-ETI.
author2 7003976733
author_facet 7003976733
Yusoff M.Z.
Al-Falahi A.
Shuaib N.H.
Yusaf T.
format Conference paper
author Yusoff M.Z.
Al-Falahi A.
Shuaib N.H.
Yusaf T.
author_sort Yusoff M.Z.
title Numerical simulations of transient flows in shock tube and validations with experimental measurements
title_short Numerical simulations of transient flows in shock tube and validations with experimental measurements
title_full Numerical simulations of transient flows in shock tube and validations with experimental measurements
title_fullStr Numerical simulations of transient flows in shock tube and validations with experimental measurements
title_full_unstemmed Numerical simulations of transient flows in shock tube and validations with experimental measurements
title_sort numerical simulations of transient flows in shock tube and validations with experimental measurements
publisher EUROSIS
publishDate 2023
_version_ 1806425498117472256
score 13.214268