Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine
Subtitle: II - effect of air ejection on turbine performance
By: Jeffery E. Haas and Milton G. Kofskey.
Contributors: Kofskey, Milton G.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical paper ; 1018; NASA technical paper -- 1018.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1977
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 35
Subjects: Aerodynamics.; Airplanes -- Turborjet engines -- Cooling.
Notes: Issued Aug. 1977.

Includes bibliographical references.