http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade
National Aeronautics and Space Administration,
1 online resource (25 pages) : illustrations.
Title from title screen (viewed Jan. 15, 2013).
"This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center."
Includes bibliographical references (pages 24-25).
Prepared under contract NNC06BA07B NNC10E420T-0 WBS 877868.02.07.03.01.02.01