NUMERICAL ANALYSIS ON THE CAVITATION IN AN INJECTOR ORIFICE
碩士 === 國立成功大學 === 航空太空工程學系 === 83 === PISO algorithm is adopted to calculate the flow field in a suddenly contracted injector orifice under a certain range of Reynolds numbers. In the present study PISO algorithm demons- trates to possess good numerical s...
Main Authors: | , |
---|---|
Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
1995
|
Online Access: | http://ndltd.ncl.edu.tw/handle/01946338735388985739 |
id |
ndltd-TW-083NCKU0295055 |
---|---|
record_format |
oai_dc |
spelling |
ndltd-TW-083NCKU02950552015-10-13T12:53:36Z http://ndltd.ncl.edu.tw/handle/01946338735388985739 NUMERICAL ANALYSIS ON THE CAVITATION IN AN INJECTOR ORIFICE 以數值方法探討注油器管內流場之空蝕現象 YING-CHI CHUO 卓英吉 碩士 國立成功大學 航空太空工程學系 83 PISO algorithm is adopted to calculate the flow field in a suddenly contracted injector orifice under a certain range of Reynolds numbers. In the present study PISO algorithm demons- trates to possess good numerical stability in using large time steps for steady flows. It also has well-accepted transient accuracy to be an alternative choice for unsteady flows. As far as the steady flow of the injector orifice is concerned, a re- circulation zone is predicted to occur in the vicinity of the entrance of the orifice to form vena contracta at certain Rey- nolds number. The length of the recirculation zone increases with the increasing Reynolds number. The local pressure, however, descends as the Reynolds number increases. Since cavitation occurs as the local pressure drops down to the vapor pressure, the minimum pressure in the flow field is predicted under various Reynolds numbers. In a comparision between this minimum pressure and the vapor pressure at the given operating condition, the flow condition at which and location where cavitation incepts are identified. TSUNG-LEO JIANG 江滄柳 1995 學位論文 ; thesis 71 zh-TW |
collection |
NDLTD |
language |
zh-TW |
format |
Others
|
sources |
NDLTD |
description |
碩士 === 國立成功大學 === 航空太空工程學系 === 83 === PISO algorithm is adopted to calculate the flow field in a
suddenly contracted injector orifice under a certain range of
Reynolds numbers. In the present study PISO algorithm demons-
trates to possess good numerical stability in using large time
steps for steady flows. It also has well-accepted transient
accuracy to be an alternative choice for unsteady flows. As far
as the steady flow of the injector orifice is concerned, a re-
circulation zone is predicted to occur in the vicinity of the
entrance of the orifice to form vena contracta at certain Rey-
nolds number. The length of the recirculation zone increases
with the increasing Reynolds number. The local pressure,
however, descends as the Reynolds number increases. Since
cavitation occurs as the local pressure drops down to the vapor
pressure, the minimum pressure in the flow field is predicted
under various Reynolds numbers. In a comparision between this
minimum pressure and the vapor pressure at the given operating
condition, the flow condition at which and location where
cavitation incepts are identified.
|
author2 |
TSUNG-LEO JIANG |
author_facet |
TSUNG-LEO JIANG YING-CHI CHUO 卓英吉 |
author |
YING-CHI CHUO 卓英吉 |
spellingShingle |
YING-CHI CHUO 卓英吉 NUMERICAL ANALYSIS ON THE CAVITATION IN AN INJECTOR ORIFICE |
author_sort |
YING-CHI CHUO |
title |
NUMERICAL ANALYSIS ON THE CAVITATION IN AN INJECTOR ORIFICE |
title_short |
NUMERICAL ANALYSIS ON THE CAVITATION IN AN INJECTOR ORIFICE |
title_full |
NUMERICAL ANALYSIS ON THE CAVITATION IN AN INJECTOR ORIFICE |
title_fullStr |
NUMERICAL ANALYSIS ON THE CAVITATION IN AN INJECTOR ORIFICE |
title_full_unstemmed |
NUMERICAL ANALYSIS ON THE CAVITATION IN AN INJECTOR ORIFICE |
title_sort |
numerical analysis on the cavitation in an injector orifice |
publishDate |
1995 |
url |
http://ndltd.ncl.edu.tw/handle/01946338735388985739 |
work_keys_str_mv |
AT yingchichuo numericalanalysisonthecavitationinaninjectororifice AT zhuōyīngjí numericalanalysisonthecavitationinaninjectororifice AT yingchichuo yǐshùzhífāngfǎtàntǎozhùyóuqìguǎnnèiliúchǎngzhīkōngshíxiànxiàng AT zhuōyīngjí yǐshùzhífāngfǎtàntǎozhùyóuqìguǎnnèiliúchǎngzhīkōngshíxiànxiàng |
_version_ |
1716868252213182464 |