Assessment of a 3-D boundary layer analysis to predict heat transfer and flow field in a turbine passage
By: by O.L. Anderson.
Contributors: United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- CR-174894.; NASA contractor report -- NASA CR-174894.
Publisher: United Technologies Research Center; National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1985
Place of publication: East Hartford, Conn; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Flow distribution.; Fluid dynamics.; Gas turbine engines.; Heat transfer.; Three dimensional boundary layer.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1988] 1 microfiche.