Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine
By: Jeffrey 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 ; 1032; 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: title: 3. Effect or rotor tip clearance on overall performance of a solid blade configuration.