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Author Ameri, Ali A., author.

Title Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade [electronic resource] / Ali A. Ameri.

Publication Info. Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:2012-217436    ---  Available
Description 1 online resource (25 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series [NASA contractor report] ; NASA-CR 2012-217436
NASA contractor report ; NASA CR-217436.
Note 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."
Bibliography Includes bibliographical references (pages 24-25).
Funding E-18129
Prepared under contract NNC06BA07B NNC10E420T-0 WBS 877868.02.07.03.01.02.01
Subject Computational fluid dynamics.
Turbulent boundary layer.
Turbine blades.
Heat transfer.
Losses.
Low reynolds number.
Pressure ratio.
Three dimensional flow.
Laminar flow.
Added Author NASA Glenn Research Center, issuing body.
Fundamental Aeronautics Program (U.S.), sponsoring body.
United States. National Aeronautics and Space Administration, sponsoring body.
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:2012-217436

 
    
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