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Source: The Open Library

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1High-lift systems on commercial subsonic airliners

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“High-lift systems on commercial subsonic airliners” Metadata:

  • Title: ➤  High-lift systems on commercial subsonic airliners
  • Author:
  • Language: English
  • Number of Pages: Median: 155
  • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

“High-lift systems on commercial subsonic airliners” 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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    2Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊

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    “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:

    • Title: ➤  Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
    • Author:
    • Language: English
    • Number of Pages: Median: 145
    • Publisher: ➤  National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  Hampton, Va - [Washington, DC - Springfield, Va

    “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” 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

    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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      3Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system

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      “Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system” Metadata:

      • Title: ➤  Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
      • Author:
      • Language: English
      • Number of Pages: Median: 112
      • Publisher: ➤  Langley Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Office
      • Publish Date:
      • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

      “Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system” 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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        4Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program

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        “Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program” Metadata:

        • Title: ➤  Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
        • 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

        “Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program” 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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          5Wing pressure distributions from subsonic tests of a high-wing transport model

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          “Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:

          • Title: ➤  Wing pressure distributions from subsonic tests of a high-wing transport model
          • 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

          “Wing pressure distributions from subsonic tests of a high-wing transport model” 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

          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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            6Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap

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            “Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap” Metadata:

            • Title: ➤  Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
            • 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

            “Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap” 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.

            Online Borrowing:

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              7Application of particle image velocimetry to a study of flow about a multi-element airfoil

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              “Application of particle image velocimetry to a study of flow about a multi-element airfoil” Metadata:

              • Title: ➤  Application of particle image velocimetry to a study of flow about a multi-element airfoil
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Aeronautics and Astronautics, Stanford University
              • Publish Date:
              • Publish Location: ➤  Stanford, Calif - [Washington, DC - Springfield, Va

              “Application of particle image velocimetry to a study of flow about a multi-element airfoil” 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.

              Online Borrowing:

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                8Active Spanwise Lift Control

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                “Active Spanwise Lift Control” Metadata:

                • Title: Active Spanwise Lift Control
                • Authors:
                • Language: English
                • Publisher: ➤  American Institute of Aeronautics & Astronautics
                • Publish Date:

                “Active Spanwise Lift Control” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 2020
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Marketplaces

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                9Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps

                By

                “Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps” Metadata:

                • Title: ➤  Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps
                • Author:
                • Language: English
                • Number of Pages: Median: 118
                • Publish Date:
                • Publish Location: Pasadena

                “Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps” Subjects and Themes:

                Edition Identifiers:

                • The Open Library ID: OL6167780M
                • Online Computer Library Center (OCLC) ID: 4019082
                • Library of Congress Control Number (LCCN): 54044252

                Access and General Info:

                • First Year Published: 1951
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Marketplaces

                Find Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps at online marketplaces:


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