Aerodynamic performances of three fan stator designs operating with rotor having tip speed of 337 meters per second and pressure ratio of 1.54/

Main Author: Gelder, Thomas F.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center
Other Authors: Schmidt, James F., Esgar, Genevieve M.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980-
Series:NASA technical paper 1610, 1614
Subjects:
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100 1 |a Gelder, Thomas F. 
245 1 0 |a Aerodynamic performances of three fan stator designs operating with rotor having tip speed of 337 meters per second and pressure ratio of 1.54/  |c Thomas F. Gelder, James F. Schmidt, and Genevieve M. Esgar 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and Technical Information Office,  |c 1980- 
300 |a τ. :  |b εικ. ;  |c 28 εκ. 
490 0 |a NASA technical paper  |v 1610, 1614 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
505 1 |a τ. 1. Experimental performance -- τ. 2. Relation of analytical code calculations to experimental performance 
650 0 |a Turbomachines  |x Aerodynamics 
650 0 |a Compressors  |x Blades 
700 1 |a Schmidt, James F. 
700 1 |a Esgar, Genevieve M. 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Office 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Office 
710 2 |a Lewis Research Center 
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