Study of boundary layer development in a two-stage low-pressure turbine
By: Daniel J. Dorney ... [et al.].
Contributors: Dorney, Daniel J.; Lewis Research Center.
Series: NASA/TM -- 1999-208913.; NASA technical memorandum -- 208913.
Publisher: National Aeronautics and Space Administration, Lewis Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Jet engines.; Two stage turbines.; Computerized simulation.; Baldwin-Lomax turbulence model.; Boundary layer transition.; Transition flow.; Flow visualization.; Boundary layer separation.; Separated flow.; Rotor blades (Turbomachinery)
Notes: Shipping list no.: 99-0471-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.