Mach number effects on turbine blade transition length prediction

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

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Bibliographic Details
Main Author: Boyle, Robert J.
Corporate Author: Lewis Research Center
Other Authors: Simon, F. F. (Frederick F.)
Format: Government Document Microfilm Book
Language:English
Published: [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], [1998]
Series:NASA technical memorandum ; 208404.
Subjects:
Mach number.
Turbine blades.
Mathematical models.
Turbulence models.
Navier-Stokes equation.
Boundary layer transition.
Description
Item Description:Shipping list number: 99-0385-M.
Physical Description:1 volume.

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