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Two-dimensional cold-air cascade study of a film-cooled turbine stator blade : IV, comparison of experimental and analyatical aerodynamic results for blade with 12 rows of 0.076-centimeter (0.030-in.-) diameter holes having streamwise ejection angles

Title:Two-dimensional cold-air cascade study of a film-cooled turbine stator blade : IV, comparison of experimental and analyatical aerodynamic results for blade with 12 rows of 0.076-centimeter (0.030-in.-) diameter holes having streamwise ejection angles
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Note:National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978
  
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Subject:Turbines -- Blades
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