Two-dimensional cold-air cascade study of a film-cooled turbine stator blade / by Herman W. Prust, Jr.

Bibliographic Details
Main Author:	Prust, Herman W.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Language:	English
Published:	[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978-
Series:	NASA technical paper ; 1204
Subjects:	Turbomachines > Aerodynamics. Aerofoils. Compressors > Blades.
Physical Description:	volumes : illustrations ; 27 cm.
Format:	Government Document Book

Contents:

5. Comparison of experimental and analytical aerodynamic results for blade with 12 rows of 0.038-centimeter-(0.015 in.) diameter coolant holes having streamwise ejection angles.