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

Bibliographic Details
Main Author:	Blair, M. F.
Corporate Authors:	United Technologies Research Center, George C. Marshall Space Flight Center
Format:	Government Document Book
Language:	English
Published:	East Hartford, Conn. : [Marshall Space Flight Center, Ala.] : United Technologies Research Center ; [National Aeronautics and Space Administration, George C. Marshall Space Flight Center] ; [1991]
Series:	NASA contractor report ; NASA CR-187693.
Subjects:	Aerodynamics. Gas turbines. Heat transfer. Rotors. Three dimensional flow. Turbine pumps. Turbulence models. Viscous flow.
Online Access:	https://purl.fdlp.gov/GPO/LPS62406

Description
Item Description:	Microform.
Physical Description:	1 volume 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.