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Author:
Rigby, D. L. (David Lester), 1963-
Title:
Heat transfer in a complex trailing edge passage for a high pressure turbine blade.
Pt. 2, Simulation results [microform] / David L. Rigby, Ronald S. Bunker.
Format:
[microform] /
Publisher:
National Aeronautics and Space AdministrationGlenn Research Center ;
Copyright Date:
2002
Description:
1 v. : ill.
Reproduction Info:
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003] 1 microfiche.
Subject:
Trailing edges (Aerodynamics)
Turbine blades.
Computerized simulation.
High pressure.
Heat transfer coefficients.
Three dimensional flow.
Other Authors:
Bunker, Ronald S.
NASA Glenn Research Center
Other Titles:
Simulation results.
Notes:
Shipping list no.: 2004-0022-M. "August 2002." "Prepared under Contract NAS3-00145." "2002-GT-30213." Cataloged from surrogate.
Series:
[NASA contractor report] ; NASA/CR-2002-211701
OCLC:
(OCoLC)56040841
Locations:
USUX851 --
Iowa State University - Parks Library
(Ames)
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