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Source: The Open Library

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Search results from The Open Library

1Two-dimensional converging-diverging rippled nozzles at transonic speeds

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“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:

  • Title: ➤  Two-dimensional converging-diverging rippled nozzles at transonic speeds
  • Author:
  • Language: English
  • Number of Pages: Median: 105
  • Publisher: ➤  Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: ➤  Hampton - Hampton, Va - [Springfield, Va

“Two-dimensional converging-diverging rippled nozzles at transonic speeds” 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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    2Assessment of dual-point drag reduction for an executive-jet modified airfoil section

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    “Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Metadata:

    • Title: ➤  Assessment of dual-point drag reduction for an executive-jet modified airfoil section
    • Author:
    • Language: English
    • Number of Pages: Median: 114
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from National Technical Information Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langly Research Center
    • Publish Date:
    • Publish Location: ➤  Hampton, Virginia - Springfield, VA - Hampton, Va - [Springfield, Va

    “Assessment of dual-point drag reduction for an executive-jet modified airfoil section” 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:

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      3High-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

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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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        4Flow characteristics about a trailing edge

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        “Flow characteristics about a trailing edge” Metadata:

        • Title: ➤  Flow characteristics about a trailing edge
        • Author:
        • Number of Pages: Median: 53
        • Publisher: ➤  Institute for Aerospace Studies - Institute for Aerospace Studies, University of Toronto
        • Publish Date:
        • Publish Location: [Downsview, Ont.]

        “Flow characteristics about a trailing edge” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1988
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        5Predicting modes of the unsteady vorticity field near the trailing edge of a blade

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        “Predicting modes of the unsteady vorticity field near the trailing edge of a blade” Metadata:

        • Title: ➤  Predicting modes of the unsteady vorticity field near the trailing edge of a blade
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service [distributor - Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
        • Publish Date:
        • Publish Location: ➤  Hanover, MD - Springfield, VA - [Cleveland, Ohio]

        “Predicting modes of the unsteady vorticity field near the trailing edge of a blade” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 2003
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

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          6Development of direct-inverse 3-D method for applied aerodynamic design and analysis

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          “Development of direct-inverse 3-D method for applied aerodynamic design and analysis” Metadata:

          • Title: ➤  Development of direct-inverse 3-D method for applied aerodynamic design and analysis
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University
          • Publish Date:
          • Publish Location: ➤  College Station, Tex - Springfield, Va - [Washington, DC

          “Development of direct-inverse 3-D method for applied aerodynamic design and analysis” 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:

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            7Heat transfer in a complex trailing edge passage for a high pressure turbine blade

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            “Heat transfer in a complex trailing edge passage for a high pressure turbine blade” Metadata:

            • Title: ➤  Heat transfer in a complex trailing edge passage for a high pressure turbine blade
            • Author:
            • Language: English
            • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
            • Publish Date:
            • Publish Location: ➤  [Cleveland, Ohio] - Hanover, MD

            “Heat transfer in a complex trailing edge passage for a high pressure turbine blade” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 2002
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

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              8A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation

              By

              “A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation” Metadata:

              • Title: ➤  A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation
              • Author:
              • Number of Pages: Median: 79
              • Publisher: Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Va

              “A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation” 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

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              9Trailing edge flow conditions as a factor in airfoil design

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              “Trailing edge flow conditions as a factor in airfoil design” Metadata:

              • Title: ➤  Trailing edge flow conditions as a factor in airfoil design
              • Author:
              • Language: English
              • Publisher: ➤  Aeronautical and Astronautical Engineering Dept., University of Illinois - National Aeronautics and Space Administration
              • Publish Date:
              • Publish Location: Urbana, Ill - [Washington, DC

              “Trailing edge flow conditions as a factor in airfoil design” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1984
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

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                10NACA 0015 wing pressure and trailing vortex measurements

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                “NACA 0015 wing pressure and trailing vortex measurements” Metadata:

                • Title: ➤  NACA 0015 wing pressure and trailing vortex measurements
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service , distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                • Publish Date:
                • Publish Location: ➤  [Springfield, Va - Washington, D.C

                “NACA 0015 wing pressure and trailing vortex measurements” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1991
                • 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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                  11Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane

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                  “Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Metadata:

                  • Title: ➤  Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service (NTIS) [distributor
                  • Publish Date:
                  • Publish Location: Springfield, VA - Hampton, Va

                  “Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” 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.

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                    12Attached and separated trailing edge flow measurements with a triple-split hot-film probe

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                    “Attached and separated trailing edge flow measurements with a triple-split hot-film probe” Metadata:

                    • Title: ➤  Attached and separated trailing edge flow measurements with a triple-split hot-film probe
                    • Author:
                    • Number of Pages: Median: 111
                    • Publisher: ➤  University of Toronto, Graduate Department of Aerospace Science and Engineering
                    • Publish Date:
                    • Publish Location: [Toronto, Ont.]

                    “Attached and separated trailing edge flow measurements with a triple-split hot-film probe” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1992
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

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                    13Optimum transonic airfoils based on the Euler equations

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                    “Optimum transonic airfoils based on the Euler equations” Metadata:

                    • Title: ➤  Optimum transonic airfoils based on the Euler equations
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - [Washington, DC

                    “Optimum transonic airfoils based on the Euler equations” 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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                      14Asymptotic behavior of a flat plate wake

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                      “Asymptotic behavior of a flat plate wake” Metadata:

                      • Title: ➤  Asymptotic behavior of a flat plate wake
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                      • Publish Date:
                      • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

                      “Asymptotic behavior of a flat plate wake” 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:

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                        Wiki

                        Source: Wikipedia

                        Wikipedia Results

                        Search Results from Wikipedia

                        Trailing edge

                        exerted by the sharp trailing edge of an aerofoil on the circulation.” Other sharp-edged surfaces that are attached to the trailing edges of wings or control

                        Flap (aeronautics)

                        aircraft wing at a given weight. Flaps are usually mounted on the wing trailing edges of a fixed-wing aircraft. Flaps are used to reduce the take-off distance

                        Chord (aeronautics)

                        edge and trailing edge of an aerofoil cross section parallel to the direction of the airflow. The chord length is the distance between the trailing edge

                        Chengdu J-36

                        one leading-edge extension (LRX) and five trailing edge control surfaces on each wing (including two split flap rudders at outboard wing edges), multiple

                        Gurney flap

                        The Gurney flap (or wickerbill) is a small tab projecting from the trailing edge of a wing. Typically it is set at a right angle to the pressure-side

                        Leading-edge slat

                        intended to operate within a wide range of speeds. Trailing-edge flap systems running along the trailing edge of the wing are common on all aircraft. Types

                        Kutta condition

                        that is applicable to solid bodies with sharp corners, such as the trailing edges of airfoils. It is named for German mathematician and aerodynamicist

                        Flight control surfaces

                        The Wright brothers used wing warping, a technique where the outer trailing edges of the wing were manipulated to control the roll. However, this technique

                        Supersonic airfoils

                        "biconvex airfoils" respectively), with very sharp leading and trailing edges. The sharp edges prevent the formation of a detached bow shock in front of the

                        ATA 100

                        581:Left Wing Trailing Edge, Outbd Aileron And Control Tab 582:Left Wing Trailing Edge Outbd Flap And Spoilers No1 - No4 583:Left Wing Trailing Edge, Inbd Aileron