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

Bibliographic Details
Main Author:	Blair, Michael F.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Anderson, Olof L.
Format:	Government Document Microform Book
Language:	English
Published:	East Hartford, Conn. : [Washington, D.C.] : United Technologies Research Center ; [National Aeronautics and Space Administration], [1989]
Series:	NASA contractor report ; NASA/CR-183891.
Subjects:	Heat transfer. High pressure. Navier-Stokes equation. Reynolds number. Rotors. Space shuttle main engine. Surface roughness. Temperature distribution. Turbine pumps.
Online Access:	https://purl.fdlp.gov/GPO/LPS69014

Description
Item Description:	"Date: November 1989." Shipping list number: 91-0122-M. Microform.
Physical Description:	1 volume Also available via Internet from the NASA Technical Report Server web site. Address as of 4/18/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900014415%5F1990014415.pdf; current access available via PURL.