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The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage / reported by M.F. Blair
Author:
Blair, M. F.
Published:
East Hartford, Connecticut : United Technologies Research Center, November 1991.
Physical Description:
1 online resource (vi, 67 pages, 172 unnumbered pages) : illustrations
Additional Creators:
United Technologies Research Center
Access Online
purl.fdlp.gov
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Series:
NASA contractor report ; NASA CR-184260
Restrictions on Access:
Free-to-read Unrestricted online access
Report Numbers:
NAS 1.26:184260
Subject(s):
Aerodynamics
Gas turbines
Heat transfer
Rotors
Three dimensional flow
Turbine pumps
Turbulence models
Viscous flow
Note:
"November 1991."
Description based on online resource; title from PDF title page (NASA, viewed Sep. 12, 2017).
Bibliography Note:
Includes bibliographical references (pages 53-57).
Type of Report and Period Covered Note:
Contractor report final.
Funding Information:
Sponsored by National Aeronautics and Space Administration, Marshall Space Flight Center NAS8-38870
UTRC R91-970057-3
View MARC record
| catkey: 21590595