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:	Wall flow. Turbocompressors. Flow visualization. Leakage. Turbomachinery.

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Call Number:	NAS 1.26:2015-218868
NAS 1.26:2015-218868	Available