東華大學圖書館 |

語系: 繁體中文

說明(常見問題)

回圖書館首頁

手機版館藏查詢

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

FindBook

Google Book

Amazon

博客來

Numerical Investigation on Flow Past a Backward Facing Step and Initial Study of Synthetic Jets.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Numerical Investigation on Flow Past a Backward Facing Step and Initial Study of Synthetic Jets./
作者:	Ho, Haonan Howard.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2021,
面頁冊數:	94 p.
附註:	Source: Masters Abstracts International, Volume: 83-06.
Contained By:	Masters Abstracts International83-06.
標題:	Mechanical engineering. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28722225
ISBN:	9798496562256

Numerical Investigation on Flow Past a Backward Facing Step and Initial Study of Synthetic Jets.
Ho, Haonan Howard.

Numerical Investigation on Flow Past a Backward Facing Step and Initial Study of Synthetic Jets. - Ann Arbor : ProQuest Dissertations & Theses, 2021 - 94 p.

Source: Masters Abstracts International, Volume: 83-06.

Thesis (M.A.S.)--University of Toronto (Canada), 2021.

This item must not be sold to any third party vendors.

The flow past a backward-facing step and the interaction of a synthetic jet with a duct cross-flow were investigated numerically using an incompressible RANS solver. The numerical result was able to predict the correct flow structure and velocity field for the backward-facing step. The synthetic jet actuator had a cylindrical cavity and the diaphragm movement was modelled physically accurate. The synthetic jet simulated was first validated with experimental data in quiescent flow, the jet velocity profile at peak phases were modelled correctly and net positive momentum was observed in the external region, while the actuator remained net-zero mass flux. The synthetic jet was then integrated into a duct to create a cross-flow, three different blowing ratios were simulated by adjusting the diaphragm vibration amplitude. The simulations allowed the formation of the synthetic jet to be analysed in a low Reynolds number cross-flow and demonstrated that URANS can be used to simulate synthetic-jet in both quiescent and cross-flow.

ISBN: 9798496562256Subjects--Topical Terms:

649730
Mechanical engineering.
Subjects--Index Terms:

Crossflow

Numerical Investigation on Flow Past a Backward Facing Step and Initial Study of Synthetic Jets.
LDR:02229nmm a2200373 4500 001 2343064
005 20220415160131.5
008 241004s2021 ||||||||||||||||| ||eng d
020 $a 9798496562256
035 $a (MiAaPQ)AAI28722225
035 $a AAI28722225
040 $a MiAaPQ $c MiAaPQ
100 1 $a Ho, Haonan Howard. $3 3681505
245 1 0 $a Numerical Investigation on Flow Past a Backward Facing Step and Initial Study of Synthetic Jets.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2021
300 $a 94 p.
500 $a Source: Masters Abstracts International, Volume: 83-06.
500 $a Includes supplementary digital materials.
500 $a Advisor: Sullivan, Pierre E.
502 $a Thesis (M.A.S.)--University of Toronto (Canada), 2021.
506 $a This item must not be sold to any third party vendors.
520 $a The flow past a backward-facing step and the interaction of a synthetic jet with a duct cross-flow were investigated numerically using an incompressible RANS solver. The numerical result was able to predict the correct flow structure and velocity field for the backward-facing step. The synthetic jet actuator had a cylindrical cavity and the diaphragm movement was modelled physically accurate. The synthetic jet simulated was first validated with experimental data in quiescent flow, the jet velocity profile at peak phases were modelled correctly and net positive momentum was observed in the external region, while the actuator remained net-zero mass flux. The synthetic jet was then integrated into a duct to create a cross-flow, three different blowing ratios were simulated by adjusting the diaphragm vibration amplitude. The simulations allowed the formation of the synthetic jet to be analysed in a low Reynolds number cross-flow and demonstrated that URANS can be used to simulate synthetic-jet in both quiescent and cross-flow.
590 $a School code: 0779.
650 4 $a Mechanical engineering. $3 649730
650 4 $a Fluid mechanics. $3 528155
650 4 $a Computational physics. $3 3343998
653 $a Crossflow
653 $a Finite Span Synthetic Jets
653 $a Turbulence modelling
653 $a URANS
690 $a 0548
690 $a 0204
690 $a 0216
710 2 $a University of Toronto (Canada). $b Mechanical and Industrial Engineering. $3 2100959
773 0 $t Masters Abstracts International $g 83-06.
790 $a 0779
791 $a M.A.S.
792 $a 2021
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28722225