Heat transfer in a complex trailing edge passage for a high pressure turbine blade.
By: David L. Rigby, Ronald S. Bunker.
Contributors: Bunker, Ronald S.; NASA Glenn Research Center.
Series: [NASA contractor report] -- NASA/CR-2002-211701.; NASA contractor report -- NASA CR-211701.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information
Published: 2002
Place of publication: [Cleveland, Ohio]; Hanover, MD
Language: eng
Format: Microform
Subjects: Trailing edges.; Turbine blades.; Computerized simulation.; High pressure.; Heat transfer coefficients.; Three dimensional flow.
Other titles: Simulation results.
Notes: Shipping list no.: 2004-0022-M.

"August 2002."

"Prepared under Contract NAS3-00145."

"2002-GT-30213."

Cataloged from surrogate.

Also available via Internet from the NASA Web site. Address as of 7/28/04: http://gltrs.grc.nasa.gov/reports/2002/CR-2002-211701.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003] 1 microfiche.