Axial-flow turbine rotor discharge-flow overexpansion and limit-loading condition. Part 1, Computational fluid dynamics (CFD) investigation /

Bibliographic Details

Main Author:	Chen, Shu-Cheng S. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2017.
Series:	NASA technical memorandum ; 2017-219506.
Subjects:	Computational fluid dynamics. Axial flow turbines. Turbine blades. formula. Supercritical flow. Critical flow.
Online Access:	https://purl.fdlp.gov/GPO/gpo83670