Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

Effect of velocity and temperature distributi ...
V. K. Garg
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Last edited by WorkBot
January 21, 2010 | History

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

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Cover of: Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades
Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades
1997, National Aeronautics and Space Administration, National Technical Information Service, distributor
Microform in English

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Book Details


Edition Notes

Shipping list no.: 99-0354-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.

Published in
[Washington, D.C, Springfield, Va
Series
NASA/TM -- 208146., NASA technical memorandum -- 208146.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL15541895M

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January 21, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page