Heat transfer in a complex trailing edge passage for a high pressure turbine blade. Pt. 2, Simulation results /

Bibliographic Details

Main Author:	Rigby, D. L. (David Lester), 1963-
Corporate Author:	NASA Glenn Research Center
Other Authors:	Bunker, Ronald S.
Format:	Government Document Microform Book
Language:	English
Published:	[Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, [2002]
Series:	NASA contractor report ; NASA CR-211701.
Subjects:	Trailing edges. Turbine blades. Computerized simulation. High pressure. Heat transfer coefficients. Three dimensional flow.
Online Access:	https://purl.fdlp.gov/GPO/LPS51556