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.

Description

Main Author

Prust, Herman W.

Related Names

Lewis Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1978.

Subjects

Turbines > Turbines / Blades.

Note

Issued Mar. 1978.

Physical Description

27 p. : ill. ; 27 cm.

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