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 -- 1338, 1659.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office
Published: 1978
Place of publication: Washington, D.C; [Springfield, Va.]
Language: eng
Subjects: Turbomachines -- Aerodynamics.; Compressors -- Aerodynamics.
Notes: "Lewis Research Center."

"Apr. 1980"-1659.

"Nov. 1979"-1338.

Bibliographies included.