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 /

Bibliographic Details

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.
Online Access:	https://purl.fdlp.gov/GPO/gpo65196 http://purl.fdlp.gov/GPO/gpo65196