Explore: Rectangular Wings

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Source: The Open Library

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1Flutter of a low-aspect-ratio rectangular wing

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“Flutter of a low-aspect-ratio rectangular wing” Metadata:

  • Title: ➤  Flutter of a low-aspect-ratio rectangular wing
  • Author:
  • Language: English
  • Number of Pages: Median: 15
  • Publisher: ➤  For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va - [Springfield, Va

“Flutter of a low-aspect-ratio rectangular wing” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1989
  • 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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    2Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7

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    “Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7” Metadata:

    • Title: ➤  Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
    • Publish Date:
    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

    “Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1989
    • 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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      3Study of the unsteady flow features on a stalled wing

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      “Study of the unsteady flow features on a stalled wing” Metadata:

      • Title: ➤  Study of the unsteady flow features on a stalled wing
      • Author:
      • Language: English
      • Publisher: ➤  American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - Reston, VA - [Washington, DC

      “Study of the unsteady flow features on a stalled wing” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1997
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

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        4Zur Berechnung der Strömung um nicht angestellte dicke Tragflügel endlicher Streckung in inkompressibler Potentialströmung

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        “Zur Berechnung der Strömung um nicht angestellte dicke Tragflügel endlicher Streckung in inkompressibler Potentialströmung” Metadata:

        • Title: ➤  Zur Berechnung der Strömung um nicht angestellte dicke Tragflügel endlicher Streckung in inkompressibler Potentialströmung
        • Author:
        • Language: ger
        • Number of Pages: Median: 129
        • Publisher: E. Lokkay
        • Publish Date:
        • Publish Location: Darmstadt

        “Zur Berechnung der Strömung um nicht angestellte dicke Tragflügel endlicher Streckung in inkompressibler Potentialströmung” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1966
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        5Cellular structures in the flow over the flap of a two-element wing

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        “Cellular structures in the flow over the flap of a two-element wing” Metadata:

        • Title: ➤  Cellular structures in the flow over the flap of a two-element wing
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Washington, DC - Springfield, Va

        “Cellular structures in the flow over the flap of a two-element wing” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1997
        • 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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          6A parametric study of accelerations of an airplane due to a wake vortex system

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          “A parametric study of accelerations of an airplane due to a wake vortex system” Metadata:

          • Title: ➤  A parametric study of accelerations of an airplane due to a wake vortex system
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: Hampton, Va - Springfield, VA

          “A parametric study of accelerations of an airplane due to a wake vortex system” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1999
          • 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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            7Some effects of aerodynamic spoilers on wing flutter

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            “Some effects of aerodynamic spoilers on wing flutter” Metadata:

            • Title: ➤  Some effects of aerodynamic spoilers on wing flutter
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
            • Publish Date:
            • Publish Location: Hampton, Va

            “Some effects of aerodynamic spoilers on wing flutter” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1989
            • 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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              8Steady and unsteady three-dimensional transonic flow computations by integral equation method

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              “Steady and unsteady three-dimensional transonic flow computations by integral equation method” Metadata:

              • Title: ➤  Steady and unsteady three-dimensional transonic flow computations by integral equation method
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
              • Publish Date:
              • Publish Location: ➤  Springfield, Va - [Washington, DC

              “Steady and unsteady three-dimensional transonic flow computations by integral equation method” 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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                9Computational test cases for a rectangular supercritical wing undergoing pitching oscillations

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                “Computational test cases for a rectangular supercritical wing undergoing pitching oscillations” Metadata:

                • Title: ➤  Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                • Publish Date:
                • Publish Location: Hampton, Va - Springfield, VA

                “Computational test cases for a rectangular supercritical wing undergoing pitching oscillations” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1999
                • 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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                  10Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing

                  By

                  “Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing” Metadata:

                  • Title: ➤  Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 27
                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - [Washington, D.C

                  “Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing” 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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                    11The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data

                    By

                    “The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data” Metadata:

                    • Title: ➤  The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                    • Publish Date:
                    • Publish Location: ➤  [Washington, D.C - Springfield, Va

                    “The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data” 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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                      12Characteristics of a rectangular wing with a peripheral jet in ground effect

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                      “Characteristics of a rectangular wing with a peripheral jet in ground effect” Metadata:

                      • Title: ➤  Characteristics of a rectangular wing with a peripheral jet in ground effect
                      • Author:
                      • Number of Pages: Median: 30
                      • Publisher: ➤  Institute for Aerospace Studies
                      • Publish Date:
                      • Publish Location: [Downsview, Ont.]

                      “Characteristics of a rectangular wing with a peripheral jet in ground effect” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1962
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

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                      13Characteristics of a rectangular wing with a peripheral jet in ground effect

                      By

                      “Characteristics of a rectangular wing with a peripheral jet in ground effect” Metadata:

                      • Title: ➤  Characteristics of a rectangular wing with a peripheral jet in ground effect
                      • Author:
                      • Number of Pages: Median: 23
                      • Publisher: ➤  Institute for Aerospace Studies
                      • Publish Date:
                      • Publish Location: [Downsview, Ont.]

                      “Characteristics of a rectangular wing with a peripheral jet in ground effect” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1961
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

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                      14Low speed wind tunnel tests on a series of rectangular wings of varying aspect ratio and aerofoil section

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                      “Low speed wind tunnel tests on a series of rectangular wings of varying aspect ratio and aerofoil section” Metadata:

                      • Title: ➤  Low speed wind tunnel tests on a series of rectangular wings of varying aspect ratio and aerofoil section
                      • Author:
                      • Language: English
                      • Number of Pages: Median: 131
                      • Publisher: H.M.S.O.
                      • Publish Date:
                      • Publish Location: London

                      “Low speed wind tunnel tests on a series of rectangular wings of varying aspect ratio and aerofoil section” Subjects and Themes:

                      Edition Identifiers:

                      • The Open Library ID: OL5585894M
                      • Online Computer Library Center (OCLC) ID: 2901297
                      • Library of Congress Control Number (LCCN): 67104321

                      Access and General Info:

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

                      Online Marketplaces

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