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

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Bibliographic Details
Author / Creator:McVetta, Ashlie B., author.
Uniform title:Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade (Revised copy)
Edition:Revised copy.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2014.
Description:1 online resource (23 pages) : color illustrations.
Language:English
Series:NASA/TM ; 2013-218070/REV1
NASA technical memorandum ; 2013-218070/REV1.
Subject:Supersonic turbines.
Turbine blades.
Aerodynamic heat transfer.
Computational fluid dynamics.
Reynolds number.
Pressure distribution.
Inlet flow.
Angles (geometry)
Angles (Geometry)
Computational fluid dynamics.
Reynolds number.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10294880
Hidden Bibliographic Details
Other authors / contributors:Giel, Paul W., author.
Welch, Gerard E., author.
NASA Glenn Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Fundamental Aeronautics Program (U.S.), sponsoring body.
Notes:Title from title screen (viewed Dec. 1, 2014).
"June 2014."
"This revised copy, numbered as NASA/TM-2013-218070/REV1, June 2014, supersedes the previous version, NASA/TM-2013-218070, August 2013, in its entirety."
"AIAA-2012-3879."
Includes bibliographical references (page 23).
Sponsored by National Aeronautics and Space Administration WBS 380046.02.03.02.01.01
E-18746-1
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2013-218070/REV.1
Description
Item Description:Title from title screen (viewed Dec. 1, 2014).
"June 2014."
"This revised copy, numbered as NASA/TM-2013-218070/REV1, June 2014, supersedes the previous version, NASA/TM-2013-218070, August 2013, in its entirety."
"AIAA-2012-3879."
Physical Description:1 online resource (23 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 23).