Cover Image

On the physics of flow separation along a low pressure turbine blade under unsteady flow conditions /

Bibliographic Details
Main Authors: Schobeiri, Meinhard (Author), Öztürk, Burak (Author), Ashpis, D. E. (David E.) (Author)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2003.
Series:NASA technical memorandum ; 2003-212290.
Subjects:
Boundary layers.
Low pressure.
Turbine blades.
Turbomachinery.
Turbulent wakes.
Unsteady flow.
Online Access:https://purl.fdlp.gov/GPO/gpo81200
Description
Item Description:"June 2003."
"Prepared for the Turbo Expo 2003 cosponsored by the American Society of Mechanical Engineers and the International Gas Turbine Institute, Atlanta, Georgia, June 16-19, 2003."
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
"GT-2003-38917."
Physical Description:1 online resource (16 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 15-16).