Mach number effects on turbine blade transition length prediction /

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

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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.

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Call Number: NAS 1.15:208404
NAS 1.15:208404 Available

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