The influence of propeller root geometries on cavitation pattern at inclined shaft condition
碩士 === 國立臺灣海洋大學 === 系統工程暨造船學系 === 96 === Due to the inclined shaft condition, the angle of attack of high-speed propeller will be increased significantly, especially at the root of the propeller, when its blade rotate to 90 degrees circumferentially. It will make root erosion easily. Countermeasures...
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ndltd-TW-096NTOU53450112016-04-27T04:11:25Z http://ndltd.ncl.edu.tw/handle/96301275270273425495 The influence of propeller root geometries on cavitation pattern at inclined shaft condition 螺槳於斜軸狀況下根部幾何形狀對空化狀態之影響 Shin-Zhou Chen 陳信州 碩士 國立臺灣海洋大學 系統工程暨造船學系 96 Due to the inclined shaft condition, the angle of attack of high-speed propeller will be increased significantly, especially at the root of the propeller, when its blade rotate to 90 degrees circumferentially. It will make root erosion easily. Countermeasures such as increasing and reducing the chordlength, adopting trailing edge truncation and cupping at propeller root, are investigated. The test condition is at inclined shaft 10°,cavitation numbers are 0.75 & 0.6 . The K-J chart will be measured and the cavitation pattern at propeller root will be photographed. From the results of the experiment, it is shown that chordlength reducing at propeller root make the cavitation easily to happen. At low cavitation number, the efficiency will be reduced remarkably. Cordlength increasing at propeller root, the cavitation would be improved at low cavitation number. Trailing edge truncation can control cavitation at propeller root efficiently. Cupping makes the cavitation stable from leading edge to trailing edge at root when the blade rotates to 90 degrees, and makes face cavitation when blade rotates to 270 degrees. Young-Zehr Kehr 柯永澤 2008 學位論文 ; thesis 65 zh-TW |
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碩士 === 國立臺灣海洋大學 === 系統工程暨造船學系 === 96 === Due to the inclined shaft condition, the angle of attack of high-speed propeller will be increased significantly, especially at the root of the propeller, when its blade rotate to 90 degrees circumferentially. It will make root erosion easily. Countermeasures such as increasing and reducing the chordlength, adopting trailing edge truncation and cupping at propeller root, are investigated. The test condition is at inclined shaft 10°,cavitation numbers are 0.75 & 0.6 . The K-J chart will be measured and the cavitation pattern at propeller root will be photographed.
From the results of the experiment, it is shown that chordlength reducing at propeller root make the cavitation easily to happen. At low cavitation number, the efficiency will be reduced remarkably. Cordlength increasing at propeller root, the cavitation would be improved at low cavitation number. Trailing edge truncation can control cavitation at propeller root efficiently. Cupping makes the cavitation stable from leading edge to trailing edge at root when the blade rotates to 90 degrees, and makes face cavitation when blade rotates to 270 degrees.
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author2 |
Young-Zehr Kehr |
author_facet |
Young-Zehr Kehr Shin-Zhou Chen 陳信州 |
author |
Shin-Zhou Chen 陳信州 |
spellingShingle |
Shin-Zhou Chen 陳信州 The influence of propeller root geometries on cavitation pattern at inclined shaft condition |
author_sort |
Shin-Zhou Chen |
title |
The influence of propeller root geometries on cavitation pattern at inclined shaft condition |
title_short |
The influence of propeller root geometries on cavitation pattern at inclined shaft condition |
title_full |
The influence of propeller root geometries on cavitation pattern at inclined shaft condition |
title_fullStr |
The influence of propeller root geometries on cavitation pattern at inclined shaft condition |
title_full_unstemmed |
The influence of propeller root geometries on cavitation pattern at inclined shaft condition |
title_sort |
influence of propeller root geometries on cavitation pattern at inclined shaft condition |
publishDate |
2008 |
url |
http://ndltd.ncl.edu.tw/handle/96301275270273425495 |
work_keys_str_mv |
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