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Source: The Open Library

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1Hot-bench simulation of the active flexible wing wind-tunnel model

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“Hot-bench simulation of the active flexible wing wind-tunnel model” Metadata:

  • Title: ➤  Hot-bench simulation of the active flexible wing wind-tunnel model
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va

“Hot-bench simulation of the active flexible wing wind-tunnel model” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1990
  • 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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    2First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains

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    “First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains” Metadata:

    • Title: ➤  First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains
    • Author:
    • Language: English
    • Number of Pages: Median: 51
    • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center
    • Publish Date:
    • Publish Location: Edwards, CA

    “First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 2012
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    3Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles

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    “Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles” Metadata:

    • Title: ➤  Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles
    • Author:
    • Language: English
    • Number of Pages: Median: 20
    • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center
    • Publish Date:
    • Publish Location: Edwards, Calif

    “Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 2010
    • 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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      4Active load control during rolling maneuvers

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      “Active load control during rolling maneuvers” Metadata:

      • Title: ➤  Active load control during rolling maneuvers
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
      • Publish Date:
      • Publish Location: Springfield, VA - Hampton, Va

      “Active load control during rolling maneuvers” 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

      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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        5Aeroelastic calculations using CFD for a typical business jet model

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        “Aeroelastic calculations using CFD for a typical business jet model” Metadata:

        • Title: ➤  Aeroelastic calculations using CFD for a typical business jet model
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
        • Publish Date:
        • Publish Location: Springfield, VA - Hampton, Va

        “Aeroelastic calculations using CFD for a typical business jet model” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1996
        • 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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          6An interactive software for conceptual wing flutter analysis and parametric study

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          “An interactive software for conceptual wing flutter analysis and parametric study” Metadata:

          • Title: ➤  An interactive software for conceptual wing flutter analysis and parametric study
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
          • Publish Date:
          • Publish Location: Hampton, Va - [Springfield, Va

          “An interactive software for conceptual wing flutter analysis and parametric study” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1996
          • 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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            7Flight measurements of surface pressures on a flexible supercritical research wing

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            “Flight measurements of surface pressures on a flexible supercritical research wing” Metadata:

            • Title: ➤  Flight measurements of surface pressures on a flexible supercritical research wing
            • Author:
            • Number of Pages: Median: 117
            • Publisher: Langley Research Center
            • Publish Date:
            • Publish Location: Hampton, Va

            “Flight measurements of surface pressures on a flexible supercritical research wing” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1985
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            8Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model

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            “Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model” Metadata:

            • Title: ➤  Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model
            • Author:
            • Language: English
            • Number of Pages: Median: 11
            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
            • Publish Date:
            • Publish Location: Hampton, Va

            “Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1990
            • 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.

            Online Borrowing:

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              9Aeroservoelastic simulation of an active flexible wing wind tunnel model

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              “Aeroservoelastic simulation of an active flexible wing wind tunnel model” Metadata:

              • Title: ➤  Aeroservoelastic simulation of an active flexible wing wind tunnel model
              • Author:
              • Number of Pages: Median: 46
              • Publisher: Langely Research Center
              • Publish Date:
              • Publish Location: Hampton, Va

              “Aeroservoelastic simulation of an active flexible wing wind tunnel model” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1996
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Marketplaces

              Find Aeroservoelastic simulation of an active flexible wing wind tunnel model at online marketplaces:


              10Response of the alliance 1 proof-of-concept airplane under gust loads

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              “Response of the alliance 1 proof-of-concept airplane under gust loads” Metadata:

              • Title: ➤  Response of the alliance 1 proof-of-concept airplane under gust loads
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for Aerospace Information
              • Publish Date:
              • Publish Location: Hanover, MD - Hampton, Va

              “Response of the alliance 1 proof-of-concept airplane under gust loads” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 2001
              • 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.

              Online Borrowing:

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                11Static aeroelastic analysis of a three-dimensional generic wing

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                “Static aeroelastic analysis of a three-dimensional generic wing” Metadata:

                • Title: ➤  Static aeroelastic analysis of a three-dimensional generic wing
                • Author:
                • Language: English
                • Number of Pages: Median: 26
                • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
                • Publish Date:
                • Publish Location: ➤  Moffett Field, Calif - Springfield, Va

                “Static aeroelastic analysis of a three-dimensional generic wing” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1990
                • 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.

                Online Borrowing:

                  Online Marketplaces

                  Find Static aeroelastic analysis of a three-dimensional generic wing at online marketplaces:


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