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

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.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
Description:1 online resource (18 pages) : color illustrations.
Language:English
Series:NASA/TM ; 2013-218070
NASA technical memorandum ; 2013-218070.
Subject:Aerodynamic heat transfer.
Computational fluid dynamics.
Flow measurement.
Inlet flow.
Supersonic turbines.
Turbine blades.
Computational fluid dynamics.
Flow meters.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10292069
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.
Notes: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."
Includes bibliographical references (page 18).
Sponsored by National Aeronautics and Space Administration WBS 380046.02.03.02.01.01
E-18746
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2013-218070

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