Mach number effects on turbine blade transition length prediction /

Bibliographic Details

Main Authors:	Boyle, Robert J. (Author), Simon, F. F. (Frederick F.) (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1998.
Series:	NASA technical memorandum ; 208404.
Subjects:	Mach number. Turbine blades. Mathematical models. Turbulence models. Navier-Stokes equation. Boundary layer transition.
Online Access:	https://purl.fdlp.gov/GPO/gpo83126