An experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor / Reid A. Berdanier and Nicole L. Key.

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Bibliographic Details
Online Access: Online Access
Online Access
Main Authors: Berdanier, Reid A. (Author), Key, Nicole L. (Author)
Corporate Author: Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
Series:NASA contractor report ; NASA CR-2015-218868.
Subjects:

MARC

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245 1 3 |a An experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor /  |c Reid A. Berdanier and Nicole L. Key. 
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500 |a "Prepared under contract NNX11AI59A." 
504 |a Includes bibliographical references (pages 141-145) 
536 |a Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center  |b NNX11AI59A. 
650 7 |a Wall flow.  |2 nasat. 
650 7 |a Turbocompressors.  |2 nasat. 
650 7 |a Flow visualization.  |2 nasat. 
650 7 |a Leakage.  |2 nasat. 
650 7 |a Turbomachinery.  |2 nasat. 
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