Heat transfer coefficients of film cooling on a rotating turbine blade model: Part II - effect of Reynolds number and rotation number

Hongwei Wu; Guoqiang Xu; Bin Yang; Zhi Tao

doi:10.1115/GT2008-50535

Heat transfer coefficients of film cooling on a rotating turbine blade model: Part II - effect of Reynolds number and rotation number

Hongwei Wu, Guoqiang Xu, Bin Yang, Zhi Tao

Northumbria University

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

7 Citations (Scopus)

Original language	English
Title of host publication	Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air
Place of Publication	New York
Publisher	American Society of Mechanical Engineers
Pages	533-541
Volume	4
ISBN (Print)	9780791843147
DOIs	https://doi.org/10.1115/GT2008-50535
Publication status	Accepted/In press - 2008
Event	ASME Turbo Expo - Berlin Duration: 1 Jan 2008 → …

Conference

Conference	ASME Turbo Expo
Period	1/01/08 → …

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 13 Climate Action

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10.1115/GT2008-50535

Cite this

@inbook{e391ef8dc752463dbb948a9bfc061721,

title = "Heat transfer coefficients of film cooling on a rotating turbine blade model: Part II - effect of Reynolds number and rotation number",

author = "Hongwei Wu and Guoqiang Xu and Bin Yang and Zhi Tao",

year = "2008",

doi = "10.1115/GT2008-50535",

language = "English",

isbn = "9780791843147",

volume = "4",

pages = "533--541",

booktitle = "Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air",

publisher = "American Society of Mechanical Engineers",

note = "ASME Turbo Expo ; Conference date: 01-01-2008",

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Wu, H, Xu, G, Yang, B & Tao, Z 2008, Heat transfer coefficients of film cooling on a rotating turbine blade model: Part II - effect of Reynolds number and rotation number. in Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air. vol. 4, American Society of Mechanical Engineers, New York, pp. 533-541, ASME Turbo Expo, 1/01/08. https://doi.org/10.1115/GT2008-50535

Heat transfer coefficients of film cooling on a rotating turbine blade model: Part II - effect of Reynolds number and rotation number. / Wu, Hongwei; Xu, Guoqiang; Yang, Bin et al.
Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air. Vol. 4 New York: American Society of Mechanical Engineers, 2008. p. 533-541.

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

TY - CHAP

T1 - Heat transfer coefficients of film cooling on a rotating turbine blade model: Part II - effect of Reynolds number and rotation number

AU - Wu, Hongwei

AU - Xu, Guoqiang

AU - Yang, Bin

AU - Tao, Zhi

PY - 2008

Y1 - 2008

UR - https://www.scopus.com/pages/publications/69949149545

U2 - 10.1115/GT2008-50535

DO - 10.1115/GT2008-50535

M3 - Chapter

SN - 9780791843147

VL - 4

SP - 533

EP - 541

BT - Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air

PB - American Society of Mechanical Engineers

CY - New York

T2 - ASME Turbo Expo

Y2 - 1 January 2008

ER -

Heat transfer coefficients of film cooling on a rotating turbine blade model: Part II - effect of Reynolds number and rotation number

Conference

UN SDGs

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