Two-dimensional cold-air cascade study of a film-cooled turbine stator blade
By: by Herman W. Prust, Jr
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1204
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Subjects: Turbomachines -- Aerodynamics; Aerofoils; Compressors -- Blades
Notes: Issued Apr. 1978

Includes bibliographical references
Table of 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