Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbine
By: Jeffrey 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 ; 1032
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Information Service
Published: 1977
Place of publication: Washington; Springfield, Va
Language: eng
Subjects: Turbines; Gas-turbines; Rotors
Notes: Issued Sept. 1977

Includes bibliographical references
Table of contents: 3. Effect or rotor tip clearance on overall performance of a solid blade configuration