Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade /

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Bibliographic Details
Author / Creator:	Ameri, Ali A., author.
Imprint:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Description:	1 online resource (25 pages) : illustrations.
Language:	English
Series:	[NASA contractor report] ; NASA-CR 2012-217436 NASA contractor report ; NASA CR-217436.
Subject:	Computational fluid dynamics. Heat -- Transmission. Laminar flow. Turbulent boundary layer.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/8964060

Hidden Bibliographic Details
Other authors / contributors:	NASA Glenn Research Center, issuing body. Fundamental Aeronautics Program (U.S.), sponsoring body. United States. National Aeronautics and Space Administration, sponsoring body.
Notes:	Title from title screen (viewed Jan. 15, 2013). "April 2012." "This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center." Includes bibliographical references (pages 24-25). E-18129 Prepared under contract NNC06BA07B NNC10E420T-0 WBS 877868.02.07.03.01.02.01
GPO item no.:	0830-H-14 (online)
Govt.docs classification:	NAS 1.26:2012-217436

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