Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
By: Kerry L. McLallin, Jeffrey E. Hass.
Contributors: Haas, Jeffrey E.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Lewis Research Center.; Propulsion Laboratory (U.S.)
Series: NASA technical paper -- 1730.; AVRADCOM technical report -- 80-09.; AVRADCOM technical report -- 80-9.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 18
Subjects: Aircraft gas-turbines -- Blades.; Aerodynamic load.; Turbines -- Aerodynamics.
Notes: "Lewis Research Center."

"Propulsion Laboratory."

Oct. 1980.

Includes bibliographical references.