Two-dimensional cold-air cascade study of a film-cooled turbine stator blade
Subtitle: IV, comparison of experimental and analyatical aerodynamic results for blade with 12 rows of 0.076-centimeter-(0.030-in.-) (0.030-in.-) diameter holes having streamwise ejection angles
By: Herman W. Prust, Jr. ; Lewis Research Center
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Lewis Research Center
Series: NASA technical paper ; 1151
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
Number of pages: 27
Subjects: Turbines -- Blades
Notes: Issued Mar. 1978

Includes bibliographical references