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 /
Herman W. Prust, Jr. ; Lewis Research Center.

APA Citation

Prust, H. W., Lewis Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office. (1978). 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. [Washington]: National Aeronautics and Space Administration, Scientific and Technical Information Office .

MLA Citation

Prust, Herman W, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office. 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. [Washington]: National Aeronautics and Space Administration, Scientific and Technical Information Office , 1978.

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