English  |  正體中文  |  简体中文  |  Items with full text/Total items : 28611/40649
Visitors : 629031      Online Users : 81
RC Version 4.0 © Powered By DSPACE, MIT. Enhanced by NTU Library IR team.
Scope Adv. Search

Please use this identifier to cite or link to this item: http://ntour.ntou.edu.tw:8080/ir/handle/987654321/49992

Title: Application of DRP scheme solving for rotating disk-driven cavity
Authors: Reui-Kuo Lin
Shun-Feng Tsai
Contributors: 國立臺灣海洋大學:輪機工程學系
Keywords: disk-driven
Reynolds number
dispersion-relation-preserving (DRP)
total variation diminishing (TVD)
topological theory
Date: 2015-02
Issue Date: 2018-09-05T06:42:49Z
Publisher: International Journal Of Computational Engineering Research (IJCER)
Abstract: Abstract: This paper is to explore when the rotating disk-driven cube container structure flow generated
by different Reynolds numbers to observe structural reasons and swirl flow field generated in the space
discretization dispersion-relation-preserving (DRP) scheme finite difference method, time item then use
total variation diminishing (TVD) Runge-Kutta method format, thereby to achieve the accuracy of its
value, the paper also use topological theory to analyze the characteristics of singularity, and draw a
three-dimensional flow field pattern thereby to observe the structure and flow of the flow field case,
with the result that the Reynolds number increased flow into the spiral point position will gradually
close the bottom of the cavity, and with the impact of an increase in the Reynolds number at the bottom
of the singular point significantly smaller.
Relation: 5(2)
URI: http://ntour.ntou.edu.tw:8080/ir/handle/987654321/49992
Appears in Collections:[輪機工程學系] 期刊論文

Files in This Item:

File Description SizeFormat

All items in NTOUR are protected by copyright, with all rights reserved.


著作權政策宣告: 本網站之內容為國立臺灣海洋大學所收錄之機構典藏,無償提供學術研究與公眾教育等公益性使用,請合理使用本網站之內容,以尊重著作權人之權益。
網站維護: 海大圖資處 圖書系統組
DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library IR team Copyright ©   - Feedback