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 , joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: 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