Heat Transfer Coefficients of Film Cooling on a Rotating Turbine Blade Model: Part II—Effects of Reynolds Number and Rotation Number

Heat Transfer Coefficients of Film Cooling on a Rotating Turbine Blade Model: Part II—Effects of Reynolds Number and Rotation Number

Author(s):

Hongwei Wu

Publication title:

Heat Transfer, Parts A and B; Volume 4

Title of ser.:

ASME Symposia Volumes

Ser. no.:

TURBO EXPO 2008(4A)

Pub. Year:

2008

Vol.:

4A

Paper no.:

GT2008-50535

Page(from):

533

Page(to):

541

Pages:

9

Pub. info.:

New York: American Society of Mechanical Engineers

ISBN:

9780791843147 [0791843149]

Language:

English

Call no.:

A11661/2008

Type:

Conference Proceedings

Details

TDL ID:	ZA00049423
Series ID:	PA00000270
Conf. info. (Name):	ASME Turbo Expo : Power for Land, Sea, and Air
Conf. info. (Number):	2008
Conf. info. (Venue):	Berlin, Germany
Conf. info. (Date):	2008.06.09-2008.06.13

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