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Source: The Open Library

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1Numerical simulation of the flow about the F-18 HARV at high angle of attack

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“Numerical simulation of the flow about the F-18 HARV at high angle of attack” Metadata:

  • Title: ➤  Numerical simulation of the flow about the F-18 HARV at high angle of attack
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C - Springfield, Va - [Washington, DC - San Jose, CA

“Numerical simulation of the flow about the F-18 HARV at high angle of attack” 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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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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    2High-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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      3Low-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.

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        4Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds

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        “Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds” Metadata:

        • Title: ➤  Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds
        • Author:
        • Language: English
        • Number of Pages: Median: 123
        • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center
        • Publish Date:
        • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, D.C.]

        “Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds” 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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          5Low speed analysis of mission adaptive flaps on a high speed civil transport configuration

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          “Low speed analysis of mission adaptive flaps on a high speed civil transport configuration” Metadata:

          • Title: ➤  Low speed analysis of mission adaptive flaps on a high speed civil transport configuration
          • 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

          “Low speed analysis of mission adaptive flaps on a high speed civil transport configuration” 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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            6Wing 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.

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              7Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport

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              “Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport” Metadata:

              • Title: ➤  Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
              • Publish Date:
              • Publish Location: ➤  Springfield, VA - Hampton, Va - Hanover, MD

              “Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 2000
              • 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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                8Theoretical studies on flapped delta wings

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                “Theoretical studies on flapped delta wings” Metadata:

                • Title: ➤  Theoretical studies on flapped delta wings
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                • Publish Date:
                • Publish Location: ➤  [Moffett Field, Calif.] - [Springfield, Va

                “Theoretical studies on flapped delta wings” 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

                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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                  9Experimental studies of a delta wing with leading edge flaps

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                  “Experimental studies of a delta wing with leading edge flaps” Metadata:

                  • Title: ➤  Experimental studies of a delta wing with leading edge flaps
                  • Author:
                  • Number of Pages: Median: 35
                  • Publisher: ➤  Joint Institute for Aeronautics and Acoustics
                  • Publish Date:
                  • Publish Location: Stanford, Calif

                  “Experimental studies of a delta wing with leading edge flaps” 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 Marketplaces

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                  10The behaviour and performance of leading edge vortex flaps

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                  “The behaviour and performance of leading edge vortex flaps” Metadata:

                  • Title: ➤  The behaviour and performance of leading edge vortex flaps
                  • Author:
                  • Publisher: ➤  College of Aeronautics, Cranfield Institute of Technology
                  • Publish Date:
                  • Publish Location: Cranfield, U.K

                  “The behaviour and performance of leading edge vortex flaps” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1986
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Marketplaces

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