Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row
By: Charles A. Farrell
Contributors: Lewis Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2030
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: 54
Subjects: Aerodynamics, Transonic; Impellers -- Dynamics
Notes: "Lewis Research Center."

"June 1982"--Cover

STAR category 02

Includes bibliographical references