DSpace university logo mark
Advanced Search
Japanese | English 

NAOSITE : Nagasaki University's Academic Output SITE > Faculty of Engineering > Articles in academic journal >

多翼ファンの全圧特性に及ぼす弦節比の影響


File Description SizeFormat
Turbo34_739.pdf448.04 kBAdobe PDFView/Open

Title: 多翼ファンの全圧特性に及ぼす弦節比の影響
Other Titles: Influence of Solidity on Total Pressure Characteristic of a Multiblade Fan
Authors: 佐々木, 壮一 / 児玉, 好雄 / 林, 秀千人 / 宇都, 太一
Authors (alternative): Sasaki, Soichi / Kodama, Yoshio / Hayashi, Hidechito / Uto, Taichi
Issue Date: 10-Dec-2006
Citation: ターボ機械 34(12), pp.739-747; 2006
Abstract: In the analytical theory, a fluid loss caused by biased flow around the impeller was proposed. The upper limit of the solidity on linear design was 2.5. The total pressure of the fan based on the analysis of the fluid loss was estimated with a reasonable validity. When the solidity of the impeller was designed large, the total pressure of the fan at the same operation point became low. The slip factor and the fluid loss of vortex flow changed corresponding with the solidity. It was experimentally proved the influence of the slip factor on the total pressure of the fan was greater than the total fluid loss.
Keywords: Fan / Design / Solidity / Performance / Fluid Loss
URI: http://hdl.handle.net/10069/20089
ISSN: 03858839
Rights: ターボ機械協会
Type: Journal Article
Text Version: publisher
Appears in Collections:Articles in academic journal

Citable URI : http://hdl.handle.net/10069/20089

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

 

Valid XHTML 1.0! Copyright © 2006-2015 Nagasaki University Library - Feedback Powerd by DSpace