Two-dimensional cold-air cascade study of a film-cooled turbine stator blade
An edition of Two-dimensional cold-air cascade study of a film-cooled turbine stator blade (1978)
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
Publish Date
1978
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office,for sale by the National Technical Information Service
Language
eng
Pages
27