Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 2.05
By: Royce D. Moore and Lonnie Reid
Contributors: Reid, Lonnie; Lewis Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper -- 1659
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1978
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 101
Subjects: Turbomachines -- Aerodynamics; Compressors -- Aerodynamics
Notes: "Lewis Research Center."

Apr. 1980

Bibliography: p. 19