The effects of Reynolds number, motor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage
By: M.F. Blair.
Contributors: United Technologies Research Center.; George C. Marshall Space Flight Center.
Series: NASA CR -- 187693.; NASA contractor report -- NASA CR-187693.
Publisher: United Technologies Research Center; National Aeronautics and Space Administration, Goerge C. Marshall Space Flight Center; National Technical Information Service, distributor
Published: 1991
Place of publication: East Hartford, Conn; [Marshall Space Flight Center, Ala; Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics.; Gas turbines.; Heat transfer.; Rotors.; Three dimensional flow.; Turbine pumps.; Turbulence models.; Viscous flow.
Notes: Also 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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991]. 3 microfiches..