Mach number effects on turbine blade transition length prediction / R.J. Boyle and F.F. Simon.

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Bibliographic Details
Online Access:	Online Access Online Access
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.

Mach number effects on turbine blade transition length prediction by Boyle, Robert J.

Published 1998

Government Document Microfilm Book