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

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