Film cooling experimental investigation of a row of cone-shaped holes

Huiren Zhu; Duchun Xu; Songling Liu; Baolong Wang

Film cooling experimental investigation of a row of cone-shaped holes

Huiren Zhu
, Duchun Xu
, Songling Liu
, Baolong Wang

动力与能源学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

5 引用（Scopus）

摘要

Local heat transfer coefficients and film cooling effectiveness of hole row downstream were measured and the influences of coolant Reynolds number and blowing rate were described. The ranges of these parameters are: the coolant reynolds number from 10,000 to 25,000 and blowing rate from 0.3 to 2.0. Measurements were performed for 26 conditions.

源语言	英语
页（从-至）	65-69
页数	5
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	19
期	3
出版状态	已出版 - 1998

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引用此

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title = "Film cooling experimental investigation of a row of cone-shaped holes",

abstract = "Local heat transfer coefficients and film cooling effectiveness of hole row downstream were measured and the influences of coolant Reynolds number and blowing rate were described. The ranges of these parameters are: the coolant reynolds number from 10,000 to 25,000 and blowing rate from 0.3 to 2.0. Measurements were performed for 26 conditions.",

author = "Huiren Zhu and Duchun Xu and Songling Liu and Baolong Wang",

year = "1998",

language = "英语",

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pages = "65--69",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

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TY - JOUR

T1 - Film cooling experimental investigation of a row of cone-shaped holes

AU - Zhu, Huiren

AU - Xu, Duchun

AU - Liu, Songling

AU - Wang, Baolong

PY - 1998

Y1 - 1998

N2 - Local heat transfer coefficients and film cooling effectiveness of hole row downstream were measured and the influences of coolant Reynolds number and blowing rate were described. The ranges of these parameters are: the coolant reynolds number from 10,000 to 25,000 and blowing rate from 0.3 to 2.0. Measurements were performed for 26 conditions.

AB - Local heat transfer coefficients and film cooling effectiveness of hole row downstream were measured and the influences of coolant Reynolds number and blowing rate were described. The ranges of these parameters are: the coolant reynolds number from 10,000 to 25,000 and blowing rate from 0.3 to 2.0. Measurements were performed for 26 conditions.

UR - https://www.scopus.com/pages/publications/0032311911

M3 - 文章

AN - SCOPUS:0032311911

SN - 1001-4055

VL - 19

SP - 65

EP - 69

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 3

ER -

Film cooling experimental investigation of a row of cone-shaped holes

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