The effects of Reynolds number, motor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage /

The effects of Reynolds number, motor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage /

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Bibliographic Details
Author / Creator:Blair, M. F.
Imprint:East Hartford, Conn. : United Technologies Research Center ; [Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; Springfield, Va. : National Technical Information Service, distributor, 1991]
Description:1 v.
Language:English
Series:NASA CR ; 187693
NASA contractor report ; NASA CR-187693.
Subject:
Aerodynamics.
Gas-turbines.
Heat -- Transmission.
Rotors.
Turbine pumps.
Viscous flow.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6556532
Hidden Bibliographic Details
Other authors / contributors:United Technologies Research Center.
George C. Marshall Space Flight Center.
Notes:Available via Internet from the NASA Technical Report Server web site. Address as of 8/2/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19920002079%5F1992002079.pdf ; current access is available via PURL.
GPO item no.:0830-H-14 (MF)
0830-H-14 (online)
Govt.docs classification:NAS 1.26:187693

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