Mach number effects on turbine blade transition length prediction
By: R.J. Boyle and F.F. Simon.
Contributors: Simon, F. F.; Lewis Research Center.
Series: NASA/TM -- 1998-208404.; NASA technical memorandum -- 208404.
Publisher: National Aeronautics and Space Administration, Lewis Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Mach number.; Turbine blades.; Mathematical models.; Turbulence models.; Navier-Stokes equation.; Boundary layer transition.
Notes: Shipping list no.: 99-0385-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.