Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds

The aerodynamics problems of train commonly come when the flow pass through train body. The increasing speed of train to achieve highly technology demands has led to increase the forces and moments and increase sensitivity of train stability and may cause the train to overturn. In this paper, two pr...

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Main Authors: Mohd. Salleh, Sufiah, Mat Ali, Mohamed Sukri, Shaikh Salim, Sheikh Ahmad Zaki, Ishak, Izuan Amin, Shirakashi, Masataka, Muhammad, Sallehuddin
Format: Conference or Workshop Item
Published: 2015
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Online Access:http://eprints.utm.my/id/eprint/63395/
https://conferencealerts.com/show-event?id=147618
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spelling my.utm.633952017-05-30T03:11:48Z http://eprints.utm.my/id/eprint/63395/ Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds Mohd. Salleh, Sufiah Mat Ali, Mohamed Sukri Shaikh Salim, Sheikh Ahmad Zaki Ishak, Izuan Amin Shirakashi, Masataka Muhammad, Sallehuddin TJ Mechanical engineering and machinery The aerodynamics problems of train commonly come when the flow pass through train body. The increasing speed of train to achieve highly technology demands has led to increase the forces and moments and increase sensitivity of train stability and may cause the train to overturn. In this paper, two prisms arranged in tandem represent a simplified model of high speed train are performed at different yaw angle ranging from 0° to 90° by using the unsteady Reynolds-Averaged Navier Stokes (URANS) equation combined with k-? SST turbulence model. The Reynolds number is 3.14x105 based on height of the train and the free stream velocity. The aerodynamic quantities such as the side force, lift force and drag force coefficient show a similar trend where the forces increase with the yaw angle until a certain critical yaw angle before start to decrease till the yaw angle of 90°. The flow structure around the train under the effect of crosswind is visualized. The vorticiticy start to form from the nose and slowly drifts away further towards the trailing edge. The two-dimensional mean streamlines on the cross-section of train at different yaw angle show that the size of vortex increase as the yaw angle increase. Time averaged pressure contour plotted on the cross section along x-axis show the variation of region between high pressure and low pressure region on the leeward and windward side of the train model that may cause train to overturn. 2015 Conference or Workshop Item PeerReviewed Mohd. Salleh, Sufiah and Mat Ali, Mohamed Sukri and Shaikh Salim, Sheikh Ahmad Zaki and Ishak, Izuan Amin and Shirakashi, Masataka and Muhammad, Sallehuddin (2015) Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds. In: The International Conference on Computational Fluid Dynamics in Research and Industry 2015, 17-19 August, 2015, Kuala Lumpur, Malaysia. https://conferencealerts.com/show-event?id=147618
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Mohd. Salleh, Sufiah
Mat Ali, Mohamed Sukri
Shaikh Salim, Sheikh Ahmad Zaki
Ishak, Izuan Amin
Shirakashi, Masataka
Muhammad, Sallehuddin
Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds
description The aerodynamics problems of train commonly come when the flow pass through train body. The increasing speed of train to achieve highly technology demands has led to increase the forces and moments and increase sensitivity of train stability and may cause the train to overturn. In this paper, two prisms arranged in tandem represent a simplified model of high speed train are performed at different yaw angle ranging from 0° to 90° by using the unsteady Reynolds-Averaged Navier Stokes (URANS) equation combined with k-? SST turbulence model. The Reynolds number is 3.14x105 based on height of the train and the free stream velocity. The aerodynamic quantities such as the side force, lift force and drag force coefficient show a similar trend where the forces increase with the yaw angle until a certain critical yaw angle before start to decrease till the yaw angle of 90°. The flow structure around the train under the effect of crosswind is visualized. The vorticiticy start to form from the nose and slowly drifts away further towards the trailing edge. The two-dimensional mean streamlines on the cross-section of train at different yaw angle show that the size of vortex increase as the yaw angle increase. Time averaged pressure contour plotted on the cross section along x-axis show the variation of region between high pressure and low pressure region on the leeward and windward side of the train model that may cause train to overturn.
format Conference or Workshop Item
author Mohd. Salleh, Sufiah
Mat Ali, Mohamed Sukri
Shaikh Salim, Sheikh Ahmad Zaki
Ishak, Izuan Amin
Shirakashi, Masataka
Muhammad, Sallehuddin
author_facet Mohd. Salleh, Sufiah
Mat Ali, Mohamed Sukri
Shaikh Salim, Sheikh Ahmad Zaki
Ishak, Izuan Amin
Shirakashi, Masataka
Muhammad, Sallehuddin
author_sort Mohd. Salleh, Sufiah
title Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds
title_short Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds
title_full Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds
title_fullStr Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds
title_full_unstemmed Aerodynamics characteristics around simplified high speed train model under the effect of crosswinds
title_sort aerodynamics characteristics around simplified high speed train model under the effect of crosswinds
publishDate 2015
url http://eprints.utm.my/id/eprint/63395/
https://conferencealerts.com/show-event?id=147618
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