Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers
By: R.J. Boyle and R. Jackson.
Contributors: Jackson, R.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 106956.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic heat transfer.; Computational fluid dynamics.; Guide vanes.; High Reynolds number.; Nozzle geometry.; Transonic flow.; Turbines.; Turbulence models.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.