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