A numerical study of the effect of wake passing on turbine blade film cooling
By: James D. Heidmann.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 107077.
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: Computational fluid dynamics.; Computational grids.; Film cooling.; Finite difference theory.; Flow distribution.; Gas turbine engines.; Heat transfer.; Three dimensional flow.; Turbine blades.; Turbulent flow.; Unsteady flow.; Viscous flow.; Wakes.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0368-M.

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