Research Catalog

Study of boundary layer development in a two-stage low-pressure turbine

Title
Study of boundary layer development in a two-stage low-pressure turbine [microform] / Daniel J. Dorney ... [et al.].
Publication
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]

Details

Additional Authors
  • Dorney, Daniel J.
  • Lewis Research Center.
Description
1 v.
Series Statement
NASA/TM ; 1999-208913
Uniform Title
NASA technical memorandum ; 208913.
Subject
  • 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)
Note
  • Shipping list no.: 99-0471-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:208913
OCLC
marcive41469899
Title
Study of boundary layer development in a two-stage low-pressure turbine [microform] / Daniel J. Dorney ... [et al.].
Imprint
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
Series
NASA/TM ; 1999-208913
NASA technical memorandum ; 208913.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.
Added Author
Dorney, Daniel J.
Lewis Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:208913
Research Call Number
READEX Microfiche NAS 1.15:208913
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