Research Catalog

Development of a turbomachinery design optimization procedure using a multiple-parameter nonlinear perturbation method

Title
Development of a turbomachinery design optimization procedure using a multiple-parameter nonlinear perturbation method [microform] / Stephen S. Stahara.
Author
Stahara, Stephen S.
Publication
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1984.

Details

Additional Authors
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Description
1 v.
Series Statement
NASA contractor report ; 3831
Uniform Title
NASA contractor report ; NASA CR-3831.
Subject
  • Airfoil profiles
  • Design analysis
  • Flow visualization
  • Optimization
  • Perturbation theory
  • Turbomachine blades
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:3831
OCLC
marcive33053029
Author
Stahara, Stephen S.
Title
Development of a turbomachinery design optimization procedure using a multiple-parameter nonlinear perturbation method [microform] / Stephen S. Stahara.
Imprint
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1984.
Series
NASA contractor report ; 3831
NASA contractor report ; NASA CR-3831.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 3 microfiches.
Added Author
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:3831
Research Call Number
READEX Microfiche NAS 1.26:3831
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