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Source: The Open Library

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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:

    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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      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

      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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        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:

        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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          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:

          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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            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

            Downloads Are Not Available:

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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

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              “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:

              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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                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:

                      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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