Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling

Shinkansen bullet train was inspired by Kingfisher beak which the nose shape design of the bullet train is streamlined, and influenced the aerodynamic consumption. Long nose shape design lead to high production cost, material usage and longer building time. Therefore, the high-profile curve design w...

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Bibliographic Details
Main Author: Md Nor Hayati, Norilani
Format: Thesis
Language:English
English
Published: 2020
Subjects:
Online Access:http://eprints.utem.edu.my/id/eprint/25360/
https://plh.utem.edu.my/cgi-bin/koha/opac-detail.pl?biblionumber=119158
Abstract Abstract here
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author Md Nor Hayati, Norilani
author_facet Md Nor Hayati, Norilani
author_sort Md Nor Hayati, Norilani
description Shinkansen bullet train was inspired by Kingfisher beak which the nose shape design of the bullet train is streamlined, and influenced the aerodynamic consumption. Long nose shape design lead to high production cost, material usage and longer building time. Therefore, the high-profile curve design which Bezier curve was applied to improve the nose shape design of Shinkansen bullet train while preserving the other specifications of Shinkansen bullet train. Cshaped transition curves was chosen to solve this problem due to its extreme curvature that able to exhibit smooth curvature. C-shaped transition curve was used to construct an improved design by applying it at the nose shape of Shinkansen. SolidWorks SimulationXpress and ANSYS Fluid Flow (FLUENT) packages are the software used to conduct linear static analysis and dynamic analysis respectively. The improved design was compared to the existing design of Shinkansen in the analysis. As a result, design with high-profile curve application shows better result in terms of Von Mises stress, displacement, velocity, and pressure. These results are been validated by using coefficient of variation and design efficiency to identify its reliability of design. Based on the linear static analysis, Von Mises stress and displacement results showed the improved design had less value compared to the existing design. This also depicted that the improved design took a longer time to undergo the failure mode. Meanwhile, in dynamic analysis, the velocity and pressure were the output parameters. The results were justified by colour indicators. Thus, the results also fulfilled the Bernoulli principle. Undoubtedly, improved design shows better result compared to existing design.
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language English
English
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spelling utem-253602021-10-05T13:37:49Z http://eprints.utem.edu.my/id/eprint/25360/ Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling Md Nor Hayati, Norilani T Technology (General) TA Engineering (General). Civil engineering (General) Shinkansen bullet train was inspired by Kingfisher beak which the nose shape design of the bullet train is streamlined, and influenced the aerodynamic consumption. Long nose shape design lead to high production cost, material usage and longer building time. Therefore, the high-profile curve design which Bezier curve was applied to improve the nose shape design of Shinkansen bullet train while preserving the other specifications of Shinkansen bullet train. Cshaped transition curves was chosen to solve this problem due to its extreme curvature that able to exhibit smooth curvature. C-shaped transition curve was used to construct an improved design by applying it at the nose shape of Shinkansen. SolidWorks SimulationXpress and ANSYS Fluid Flow (FLUENT) packages are the software used to conduct linear static analysis and dynamic analysis respectively. The improved design was compared to the existing design of Shinkansen in the analysis. As a result, design with high-profile curve application shows better result in terms of Von Mises stress, displacement, velocity, and pressure. These results are been validated by using coefficient of variation and design efficiency to identify its reliability of design. Based on the linear static analysis, Von Mises stress and displacement results showed the improved design had less value compared to the existing design. This also depicted that the improved design took a longer time to undergo the failure mode. Meanwhile, in dynamic analysis, the velocity and pressure were the output parameters. The results were justified by colour indicators. Thus, the results also fulfilled the Bernoulli principle. Undoubtedly, improved design shows better result compared to existing design. 2020 Thesis NonPeerReviewed text en http://eprints.utem.edu.my/id/eprint/25360/1/Shape%20preserving%20in%20aerodynamic%20product%20profiles%20using%20geometric%20design%20modelling.pdf text en http://eprints.utem.edu.my/id/eprint/25360/2/Shape%20preserving%20in%20aerodynamic%20product%20profiles%20using%20geometric%20design%20modelling.pdf Md Nor Hayati, Norilani (2020) Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling. Masters thesis, Universiti Teknikal Malaysia Melaka. https://plh.utem.edu.my/cgi-bin/koha/opac-detail.pl?biblionumber=119158
spellingShingle T Technology (General)
TA Engineering (General). Civil engineering (General)
Md Nor Hayati, Norilani
Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling
thesis_level Master
title Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling
title_full Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling
title_fullStr Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling
title_full_unstemmed Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling
title_short Shape Preserving In Aerodynamic Product Profiles Using Geometric Design Modelling
title_sort shape preserving in aerodynamic product profiles using geometric design modelling
topic T Technology (General)
TA Engineering (General). Civil engineering (General)
url http://eprints.utem.edu.my/id/eprint/25360/
https://plh.utem.edu.my/cgi-bin/koha/opac-detail.pl?biblionumber=119158
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