Aerodynamic performances of three fan stator designs operating with rotor having tip speed of 337 meters per second and pressure ratio of 1.54
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Author
Contributions
- Schmidt, James F. - Contributor
- Esgar, Genevieve M. - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Office. - Contributor
- Lewis Research Center. - Contributor
Publication
1980 - National Aeronautics and Space Administration, Scientific and Technical Information Office, Washington, D.C, District of Columbia
Language
English
Subjects
Series Statement
- NASA technical paper -- 1610, 1614.
Other Editions
- Aerodynamic performances of three fan stator designs operating with rotor having tip speed of 337 meters per second and pressure ratio of 1.54
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