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Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade /

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Bibliographic Details
Main Authors: McVetta, Ashlie B. (Author), Giel, P. W. (Paul W.) (Author), Welch, Gerard E. (Author)
Corporate Author: United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
Series:NASA technical memorandum ; 2013-218070.
Subjects:
Aerodynamic heat transfer.
Computational fluid dynamics.
Flow measurement.
Inlet flow.
Supersonic turbines.
Turbine blades.
Online Access:https://purl.fdlp.gov/GPO/gpo50526
http://purl.fdlp.gov/GPO/gpo50526
Description
Item Description:Title from title screen (viewed July 9, 2014).
"August 2013."
"Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 29-August 1, 2012."
"AIAA-2012-3879."
Physical Description:1 online resource (18 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 18).