Aerodynamic performances of three fan stator designs operating with rotor having tip speed of 337 meters per second and pressure ratio of 1.54
By: Thomas F. Gelder, James F. Schmidt, and Genevieve M. Esgar
Contributors: Schmidt, James F; Esgar, Genevieve M; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Lewis Research Center
Series: NASA technical paper -- 1610, 1614
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Turbomachines -- Aerodynamics; Compressors -- Blades
Notes: "Lewis Research Center."

STAR category 07

Includes bibliographical references
Table of contents: value: v. 1. Experimental performance; value: v. 2. Relation of analytical code calculations to experimental performance