Experimental investigation of loss reduction with riblets on cascade blade surfaces and isolated airfoils

Chen Fang; Tang Yan-Ping; Chen Mao-Zhang

Experimental investigation of loss reduction with riblets on cascade blade surfaces and isolated airfoils

Chen Fang^*
, Tang Yan-Ping
, Chen Mao-Zhang

^*此作品的通讯作者

Chinese Academy of Sciences

科研成果: 期刊稿件 › 会议文章 › 同行评审

2 引用（Scopus）

摘要

Experimental investigations of loss reduction with riblets have been made. Riblets were put on the blade surfaces in different ways in a compressor cascade or on an isolated airfoil. More than 8% drag reduction benefits for an isolated airfoil and more than 10% loss reduction benefits for the compressor cascade have been obtained by using riblets only on blade pressure surfaces rather than on both pressure and suction surfaces. The mechanism underlying these results has been discussed.

源语言	英语
页（从-至）	GT207 6p
期刊	American Society of Mechanical Engineers (Paper)
出版状态	已出版 - 1990
已对外发布	是
活动	International Gas Turbine and Aeroengine Congress and Exposition - Brussels, Belg 期限: 11 6月 1990 → 14 6月 1990

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引用此

@article{bcb1c549e5b742f9a31e8810c0a7c375,

title = "Experimental investigation of loss reduction with riblets on cascade blade surfaces and isolated airfoils",

abstract = "Experimental investigations of loss reduction with riblets have been made. Riblets were put on the blade surfaces in different ways in a compressor cascade or on an isolated airfoil. More than 8\% drag reduction benefits for an isolated airfoil and more than 10\% loss reduction benefits for the compressor cascade have been obtained by using riblets only on blade pressure surfaces rather than on both pressure and suction surfaces. The mechanism underlying these results has been discussed.",

author = "Chen Fang and Tang Yan-Ping and Chen Mao-Zhang",

year = "1990",

language = "英语",

pages = "GT207 6p",

journal = "American Society of Mechanical Engineers (Paper)",

issn = "0402-1215",

note = "International Gas Turbine and Aeroengine Congress and Exposition ; Conference date: 11-06-1990 Through 14-06-1990",

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TY - JOUR

T1 - Experimental investigation of loss reduction with riblets on cascade blade surfaces and isolated airfoils

AU - Fang, Chen

AU - Yan-Ping, Tang

AU - Mao-Zhang, Chen

PY - 1990

Y1 - 1990

N2 - Experimental investigations of loss reduction with riblets have been made. Riblets were put on the blade surfaces in different ways in a compressor cascade or on an isolated airfoil. More than 8% drag reduction benefits for an isolated airfoil and more than 10% loss reduction benefits for the compressor cascade have been obtained by using riblets only on blade pressure surfaces rather than on both pressure and suction surfaces. The mechanism underlying these results has been discussed.

AB - Experimental investigations of loss reduction with riblets have been made. Riblets were put on the blade surfaces in different ways in a compressor cascade or on an isolated airfoil. More than 8% drag reduction benefits for an isolated airfoil and more than 10% loss reduction benefits for the compressor cascade have been obtained by using riblets only on blade pressure surfaces rather than on both pressure and suction surfaces. The mechanism underlying these results has been discussed.

UR - https://www.scopus.com/pages/publications/17544403589

M3 - 会议文章

AN - SCOPUS:17544403589

SN - 0402-1215

SP - GT207 6p

JO - American Society of Mechanical Engineers (Paper)

JF - American Society of Mechanical Engineers (Paper)

T2 - International Gas Turbine and Aeroengine Congress and Exposition

Y2 - 11 June 1990 through 14 June 1990

ER -

Experimental investigation of loss reduction with riblets on cascade blade surfaces and isolated airfoils

摘要

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