Navier-Stokes analysis of turbine blade heat transfer
By: R.J. Boyle ; prepared for the 35th International Gas Turbine and Aeroengine Congress and Exposition sponsored by the American Society of Mechanical Engineers, Brussels, Belgium, June 11-14, 1990.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 102496.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 19
Subjects: Turbines -- Blades.; Heat -- Transmission.; Aerothermodynamics.; Heat transfer.; Navier-Stokes equation.; Reynolds number.; Separated flow.; Turbine blades.; Vanes.
Other titles: Navier Stokes analysis of turbine blade heat transfer.
Notes: Cover title.

Shipping list no.: 90-0858-M.

"Performing organization report no.: E-5219"--Technical rept. documentation p.

Includes bibliographical references (p. 8-9).

Also available via Internet from the NASA Technical Report Server web site. Address as of 2/13/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011984%5F1990011984.pdf; current access available via PURL.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

505-62-21.