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Transonic Shock Oscillations and Wing Flutter Calculated With an Interactive Boundary Layer Coupling Method

John W. Edwards
Format
EBook; Book; Government Document; Online
Published
[Washington, DC] : [National Aeronautics and Space Administration], [1996]
Language
English
Series
NASA-TM
NASA Technical Memorandum
SuDoc Number
NAS 1.15:110484
Description
1 online resource (16 pages) : illustrations.
Notes
  • "EUROMECH-ColIoquium 349 Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 16-18, 1996."
  • Includes bibliographical references (pages 15-16).
Series Statement
NASA-TM ; 110484
NASA technical memorandum ; 110484
Copyright Not EvaluatedCopyright Not Evaluated
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Includes bibliographical references (pages 15-16).
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    a| Separated flow. 2| nasat
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    7
    a| Transonic flow. 2| nasat
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    a| Transonic flutter. 2| nasat
    650
      
    7
    a| Transonic speed. 2| nasat
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    7
    a| Unsteady flow. 2| nasat
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    7
    a| Viscous flow. 2| nasat
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    7
    a| Computational fluid dynamics. 2| nasat
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    7
    a| Coupling. 2| nasat
    650
      
    7
    a| Airfoils. 2| nasat
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    a| Mach number. 2| nasat
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    7
    a| Boundary layer separation. 2| nasat
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    a| Airfoil oscillations. 2| nasat
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