Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade /
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Author / Creator: | McVetta, Ashlie B., author. |
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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 |
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." |
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Physical Description: | 1 online resource (23 pages) : color illustrations. |
Bibliography: | Includes bibliographical references (page 23). |