Cover Image

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
Description
Item Description:Title from title screen (viewed Feb. 10, 2016).
"September 2015."
"Prepared under contract NNX11AI59A."
Physical Description:1 online resource (xiv, 145 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 141-145).