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
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