Research Catalog

Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading

Title
Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading [microform] / Nelson L. Sanger and Raymond P. Shreeve.
Author
Sanger, Nelson L.
Publication
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]

Details

Additional Authors
  • Shreeve, Raymond P.
  • Lewis Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 87167
Subject
  • Compressors > Blades
  • Gas-turbines
  • Boundary layers
  • Cascade flow
  • Comparison
  • Compressor blades
  • Compressors
  • Computation
  • Diffusion
  • Experimentation
  • Gas turbine engines
  • Inviscid flow
  • Reynolds number
  • Stators
  • Surface layers
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.15:87167
OCLC
marcive166141052
Author
Sanger, Nelson L.
Title
Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading [microform] / Nelson L. Sanger and Raymond P. Shreeve.
Imprint
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
Series
NASA technical memorandum ; 87167
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.
Added Author
Shreeve, Raymond P.
Lewis Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:87167
Research Call Number
GPO Microfiche NAS 1.15:87167
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