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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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.
Description
Item Description:"June 1998."
"Prepared for the Turbo Expo '98 sponsored by the American Society of Mechanical Engineers, Stockholm, Sweden, June 2-5, 1998."
"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
"98-GT-367."
Physical Description:1 online resource (12 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 11-12)

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