Experimental Investigation on Flow in Pin-Fin Trapezoidal Duct

Li Zhang; Hui Ren Zhu; Song Ling Liu; Xue Wen Wang; Du Chun Xu

Experimental Investigation on Flow in Pin-Fin Trapezoidal Duct

Li Zhang, Hui Ren Zhu, Song Ling Liu, Xue Wen Wang, Du Chun Xu

School of Power and Energy

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

Abstract

Experiments were conducted to determine the distribution of static pressure and lateral mass flow rate in a pin-fin trapezoidal duct that modeled the cooling passages in the gas turbine blades. The ratio of lateral-to-total flow rate was 1.The flow Reynolds numbers were varied from 1.5 × 10⁴ through 9 × 10⁴. The results show that the pressure drops along chord wise passages are much larger than that along radials. The lateral flow rates near the root and the tip of the blade are larger than that in the middle part by 5%-30%.

Original language	English
Pages (from-to)	518-521
Number of pages	4
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	21
Issue number	3
State	Published - Jun 2006

Keywords

Aerospace propulsion system
Flow
Mass flow rate
Pin-fin
Pressure

Cite this

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title = "Experimental Investigation on Flow in Pin-Fin Trapezoidal Duct",

abstract = "Experiments were conducted to determine the distribution of static pressure and lateral mass flow rate in a pin-fin trapezoidal duct that modeled the cooling passages in the gas turbine blades. The ratio of lateral-to-total flow rate was 1.The flow Reynolds numbers were varied from 1.5 × 104 through 9 × 104. The results show that the pressure drops along chord wise passages are much larger than that along radials. The lateral flow rates near the root and the tip of the blade are larger than that in the middle part by 5%-30%.",

keywords = "Aerospace propulsion system, Flow, Mass flow rate, Pin-fin, Pressure",

author = "Li Zhang and Zhu, {Hui Ren} and Liu, {Song Ling} and Wang, {Xue Wen} and Xu, {Du Chun}",

year = "2006",

month = jun,

language = "英语",

volume = "21",

pages = "518--521",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

issn = "1000-8055",

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number = "3",

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T1 - Experimental Investigation on Flow in Pin-Fin Trapezoidal Duct

AU - Zhang, Li

AU - Zhu, Hui Ren

AU - Liu, Song Ling

AU - Wang, Xue Wen

AU - Xu, Du Chun

PY - 2006/6

Y1 - 2006/6

N2 - Experiments were conducted to determine the distribution of static pressure and lateral mass flow rate in a pin-fin trapezoidal duct that modeled the cooling passages in the gas turbine blades. The ratio of lateral-to-total flow rate was 1.The flow Reynolds numbers were varied from 1.5 × 104 through 9 × 104. The results show that the pressure drops along chord wise passages are much larger than that along radials. The lateral flow rates near the root and the tip of the blade are larger than that in the middle part by 5%-30%.

AB - Experiments were conducted to determine the distribution of static pressure and lateral mass flow rate in a pin-fin trapezoidal duct that modeled the cooling passages in the gas turbine blades. The ratio of lateral-to-total flow rate was 1.The flow Reynolds numbers were varied from 1.5 × 104 through 9 × 104. The results show that the pressure drops along chord wise passages are much larger than that along radials. The lateral flow rates near the root and the tip of the blade are larger than that in the middle part by 5%-30%.

KW - Aerospace propulsion system

KW - Flow

KW - Mass flow rate

KW - Pin-fin

KW - Pressure

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M3 - 文章

AN - SCOPUS:33747449183

SN - 1000-8055

VL - 21

SP - 518

EP - 521

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 3

ER -

Experimental Investigation on Flow in Pin-Fin Trapezoidal Duct

Abstract

Keywords

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