Explore: Oscillating Wings (aerodynamics)

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Source: The Open Library

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1Application of model control to wing-flutter suppression

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“Application of model control to wing-flutter suppression” Metadata:

  • Title: ➤  Application of model control to wing-flutter suppression
  • Author:
  • Language: English
  • Number of Pages: Median: 71
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Washington, D.C

“Application of model control to wing-flutter suppression” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1982
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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2Historical background and design evolution of the transonic aircraft technology supercritical wing

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“Historical background and design evolution of the transonic aircraft technology supercritical wing” Metadata:

  • Title: ➤  Historical background and design evolution of the transonic aircraft technology supercritical wing
  • Author:
  • Language: English
  • Number of Pages: Median: 30
  • Publisher: ➤  National Aeronautical and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  Washington, D.C - [Springfield, Va

“Historical background and design evolution of the transonic aircraft technology supercritical wing” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1981
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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3The NYU inverse swept wing code

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“The NYU inverse swept wing code” Metadata:

  • Title: ➤  The NYU inverse swept wing code
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Courant Institute of Mathematical Sciences, New York University - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C - Springfield, Va - New York, N.Y

“The NYU inverse swept wing code” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1983
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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    4The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory

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    “The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory” Metadata:

    • Title: ➤  The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory
    • Author:
    • Language: English
    • Number of Pages: Median: 43
    • Publisher: H.M.S.O.
    • Publish Date:
    • Publish Location: London

    “The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory” Subjects and Themes:

    Edition Identifiers:

    • The Open Library ID: OL5570853M
    • Online Computer Library Center (OCLC) ID: 6188515
    • Library of Congress Control Number (LCCN): 67078953

    Access and General Info:

    • First Year Published: 1967
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    5The separated flows on slender wings in unsteady motion

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    “The separated flows on slender wings in unsteady motion” Metadata:

    • Title: ➤  The separated flows on slender wings in unsteady motion
    • Author:
    • Language: English
    • Number of Pages: Median: 36
    • Publisher: H.M.S.O.
    • Publish Date:
    • Publish Location: London

    “The separated flows on slender wings in unsteady motion” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1967
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    6Specialists Meeting on Wing-with-Stores Flutter

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    “Specialists Meeting on Wing-with-Stores Flutter” Metadata:

    • Title: ➤  Specialists Meeting on Wing-with-Stores Flutter
    • Author: ➤  
    • Language: English
    • Number of Pages: Median: 128
    • Publisher: ➤  North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development
    • Publish Date:
    • Publish Location: [Neuilly-sur-Seine, France]

    “Specialists Meeting on Wing-with-Stores Flutter” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1975
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    7Extracting energy from unsteady flows through vortex control

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    “Extracting energy from unsteady flows through vortex control” Metadata:

    • Title: ➤  Extracting energy from unsteady flows through vortex control
    • Author:
    • Language: English
    • Number of Pages: Median: 139
    • Publisher: ➤  Woods Hole Oceanographic Institution
    • Publish Date:
    • Publish Location: Woods Hole, Mass

    “Extracting energy from unsteady flows through vortex control” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1994
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    8Historical background and design evolution of the transonic aircraft technology supercritical wing

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    “Historical background and design evolution of the transonic aircraft technology supercritical wing” Metadata:

    • Title: ➤  Historical background and design evolution of the transonic aircraft technology supercritical wing
    • Author:
    • Language: English
    • Number of Pages: Median: 30
    • Publisher: ➤  National Aeronautical and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - [Springfield, Va

    “Historical background and design evolution of the transonic aircraft technology supercritical wing” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1981
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    9Effects of angle of attack and ventral fin on transonic flutter characteristics of an arrow-wing configuration

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    “Effects of angle of attack and ventral fin on transonic flutter characteristics of an arrow-wing configuration” Metadata:

    • Title: ➤  Effects of angle of attack and ventral fin on transonic flutter characteristics of an arrow-wing configuration
    • Author:
    • Language: English
    • Number of Pages: Median: 26
    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - [Springfield, Va

    “Effects of angle of attack and ventral fin on transonic flutter characteristics of an arrow-wing configuration” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1980
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    10Analysis of oscillatory motion of a light airplane at high values of lift coefficient

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    “Analysis of oscillatory motion of a light airplane at high values of lift coefficient” Metadata:

    • Title: ➤  Analysis of oscillatory motion of a light airplane at high values of lift coefficient
    • Author:
    • Language: English
    • Number of Pages: Median: 48
    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
    • Publish Date:
    • Publish Location: ➤  [Springfield Va - Washington, D.C

    “Analysis of oscillatory motion of a light airplane at high values of lift coefficient” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1983
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    11Comparison of analytical and experimental steady- and unsteady-pressure distributions at Mach number 0.78 for a high-aspect-ratio supercritical wing model with oscillating control surfaces

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    “Comparison of analytical and experimental steady- and unsteady-pressure distributions at Mach number 0.78 for a high-aspect-ratio supercritical wing model with oscillating control surfaces” Metadata:

    • Title: ➤  Comparison of analytical and experimental steady- and unsteady-pressure distributions at Mach number 0.78 for a high-aspect-ratio supercritical wing model with oscillating control surfaces
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va

    “Comparison of analytical and experimental steady- and unsteady-pressure distributions at Mach number 0.78 for a high-aspect-ratio supercritical wing model with oscillating control surfaces” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1983
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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      12Pressure measurements over a stationary and oscillating rectangular wing

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      “Pressure measurements over a stationary and oscillating rectangular wing” Metadata:

      • Title: ➤  Pressure measurements over a stationary and oscillating rectangular wing
      • Author:
      • Language: English
      • Number of Pages: Median: 151
      • Publish Date:

      “Pressure measurements over a stationary and oscillating rectangular wing” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1993
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

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      13Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment

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      “Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment” Metadata:

      • Title: ➤  Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
      • Publish Date:
      • Publish Location: ➤  [Washington, D.C.] - Springfield, Va

      “Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1987
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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        14Influence of display and control compatibility on pilot-induced oscillations

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        “Influence of display and control compatibility on pilot-induced oscillations” Metadata:

        • Title: ➤  Influence of display and control compatibility on pilot-induced oscillations
        • Author:
        • Language: English
        • Number of Pages: Median: 37
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
        • Publish Date:
        • Publish Location: ➤  Washington, D.C - [Springfield, Va

        “Influence of display and control compatibility on pilot-induced oscillations” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1981
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        15Application of model control to wing-flutter suppression

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        “Application of model control to wing-flutter suppression” Metadata:

        • Title: ➤  Application of model control to wing-flutter suppression
        • Author:
        • Language: English
        • Number of Pages: Median: 71
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
        • Publish Date:
        • Publish Location: ➤  Washington, D.C - [Springfield, Va

        “Application of model control to wing-flutter suppression” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1982
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        16AGARD standard aeroelastic configurations for dynamic response

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        “AGARD standard aeroelastic configurations for dynamic response” Metadata:

        • Title: ➤  AGARD standard aeroelastic configurations for dynamic response
        • Author:
        • Language: English
        • Number of Pages: Median: 74
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, Va - [Springfield, Va

        “AGARD standard aeroelastic configurations for dynamic response” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1987
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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          17Application of Zimmerman flutter-margin criterion to a wind-tunnel model

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          “Application of Zimmerman flutter-margin criterion to a wind-tunnel model” Metadata:

          • Title: ➤  Application of Zimmerman flutter-margin criterion to a wind-tunnel model
          • Author:
          • Language: English
          • Number of Pages: Median: 27
          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - Washington, D.C

          “Application of Zimmerman flutter-margin criterion to a wind-tunnel model” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1982
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          18Zur experimentellen Prüfung instationärer dreidimensionaler Tragflächentheorien bei inkompressibler Strömung

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          “Zur experimentellen Prüfung instationärer dreidimensionaler Tragflächentheorien bei inkompressibler Strömung” Metadata:

          • Title: ➤  Zur experimentellen Prüfung instationärer dreidimensionaler Tragflächentheorien bei inkompressibler Strömung
          • Author:
          • Language: ger
          • Number of Pages: Median: 114
          • Publisher: ➤  (Max-Planck-Institut für Strömungsforschung und Aerodynamische Versuchsanstalt)
          • Publish Date:
          • Publish Location: Göttingen

          “Zur experimentellen Prüfung instationärer dreidimensionaler Tragflächentheorien bei inkompressibler Strömung” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1967
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          19Teorii͡a nesushcheĭ poverkhnosti

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          Book's cover

          “Teorii͡a nesushcheĭ poverkhnosti” Metadata:

          • Title: ➤  Teorii͡a nesushcheĭ poverkhnosti
          • Author:
          • Language: rus
          • Number of Pages: Median: 159
          • Publisher: Nauka, Fizmatlit
          • Publish Date:
          • Publish Location: Moskva

          “Teorii͡a nesushcheĭ poverkhnosti” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1995
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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