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

Bibliographic Details
Main Author:	Ameri, Ali A. (Author)
Corporate Authors:	Fundamental Aeronautics Program (U.S.) (sponsoring body.), United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA contractor report ; NASA CR-217436.
Subjects:	Computational fluid dynamics. Turbulent boundary layer. Turbine blades. Heat transfer. Losses. Low Reynolds number. Pressure ratio. Three dimensional flow. Laminar flow.
Online Access:	https://purl.fdlp.gov/GPO/gpo32880

Description
Item Description:	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."
Physical Description:	1 online resource (25 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 24-25).