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A Rapid Perturbation Procedure for Determining Nonlinear Flow Solutions: Application to Transonic Turbomachinery Flows

Stephen S. Stahara, James P. Elliott, and John R. Spreiter
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Language
English
Series
NASA Contractor Report
SuDoc Number
NAS 1.26:3425
Description
iv, 90 p. : ill. ; 27 cm.
Notes
  • "Prepared for Lewis Research Center under contract NAS3-20836."
  • "May 1981"-- Cover.
  • Includes bibliographical references.
Series Statement
NASA contractor report 3425
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| A rapid perturbation procedure for determining nonlinear flow solutions : b| application to transonic turbomachinery flows / c| Stephen S. Stahara, James P. Elliott, and John R. Spreiter.
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    a| Includes bibliographical references.
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    a| Singular perturbations (Mathematics)
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    a| Turbomachines x| Blades x| Design and construction.
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    a| Elliott, J. P. q| (James Philip), d| 1929-
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