Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage/

Main Author: Moore, Royce D.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Lewis Research Center
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982
Series:NASA technical paper 2049
Subjects:
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245 1 0 |a Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage/  |c Royce D. Moore ; Lewis Research Center 
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490 0 |a NASA technical paper  |v 2049 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Rotors (Helicopters) 
650 0 |a Impellers  |x Dynamics 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Branch 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch 
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