Research Catalog

A final report on NASA grant NSG 3079 entitled A linearized Euler analysis of unsteady flows in turbomachinery

Title
A final report on NASA grant NSG 3079 entitled A linearized Euler analysis of unsteady flows in turbomachinery [microform] / by Kenneth C. Hall and Edward F. Crawley.
Author
Hall, Kenneth C.
Publication
Cambridge, MA : Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]

Details

Additional Authors
  • Crawley, Edward F.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA contractor report ; NASA CR-180987
Alternative Title
Linearized Euler analysis of unsteady flows in turbomachinery
Subject
  • Cascade flow
  • Computational fluid dynamics
  • Eular equations of motion
  • Linearization
  • Shock waves
  • Turbine blades
  • Turbomachinery
  • Unsteady flow
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:180987
OCLC
marcive32951416
Author
Hall, Kenneth C.
Title
A final report on NASA grant NSG 3079 entitled A linearized Euler analysis of unsteady flows in turbomachinery [microform] / by Kenneth C. Hall and Edward F. Crawley.
Imprint
Cambridge, MA : Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
Series
NASA contractor report ; NASA CR-180987
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1987] 2 microfiches.
Added Author
Crawley, Edward F.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:180987
Research Call Number
READEX Microfiche NAS 1.26:180987
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