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 Authors:	United States. National Aeronautics and Space Administration (sponsoring body.), Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2014.
Edition:	Revised copy.
Series:	NASA technical memorandum ; 2013-218070/REV1.
Subjects:	Supersonic turbines. Turbine blades. Aerodynamic heat transfer. Computational fluid dynamics. Reynolds number. Pressure distribution. Inlet flow. Angles (geometry)
Online Access:	https://purl.fdlp.gov/GPO/gpo53624 http://purl.fdlp.gov/GPO/gpo53624