Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, 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 Branch
Series: NASA technical paper -- 2001
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 113
Subjects: Turbomachines -- Aerodynamics; Compressors -- Aerodynamics
Notes: "Lewis Research Center."

"April 1982"--Cover

STAR category 07