Effect of rotor meridional velocity ratio on response to inlet radial and circumferential distortion
By: Nelson L. Sanger
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Lewis Research Center
Series: NASA technical paper -- 1278
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 69
Subjects: Turbomachines -- Aerodynamics; Impellers -- Dynamics
Notes: "Lewis Research Center, Cleveland, Ohio."

"July 1979"--Cover