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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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    2In-flight transport performance optimization

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    “In-flight transport performance optimization” Metadata:

    • Title: ➤  In-flight transport performance optimization
    • Author:
    • Language: English
    • Number of Pages: Median: 15
    • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Edwards, Calif

    “In-flight transport performance optimization” 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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      3In-flight investigation of shuttle tile pressure orifice installations

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      “In-flight investigation of shuttle tile pressure orifice installations” Metadata:

      • Title: ➤  In-flight investigation of shuttle tile pressure orifice installations
      • Author:
      • Language: English
      • Number of Pages: Median: 33
      • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service - Ames Research Center
      • Publish Date:
      • Publish Location: ➤  Washington, D.C - Springfield, Va - Edwards, Calif

      “In-flight investigation of shuttle tile pressure orifice installations” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1990
      • 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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        4Effects of winglets on a first-generation jet transport wing

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        “Effects of winglets on a first-generation jet transport wing” Metadata:

        • Title: ➤  Effects of winglets on a first-generation jet transport wing
        • Author:
        • Language: English
        • Number of Pages: Median: 56
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service] - Dryden Flight Research Facility
        • Publish Date:
        • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va - Edwards, Calif

        “Effects of winglets on a first-generation jet transport wing” 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 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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          5Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature

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          “Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature” Metadata:

          • Title: ➤  Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature
          • Author:
          • Language: English
          • Number of Pages: Median: 35
          • 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, D.C.] - Springfield, VA

          “Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature” 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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            6An overview of an experimental demonstration aerotow program

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            “An overview of an experimental demonstration aerotow program” Metadata:

            • Title: ➤  An overview of an experimental demonstration aerotow program
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - Edwards, Calif

            “An overview of an experimental demonstration aerotow program” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1998
            • 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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              7Active load control during rolling maneuvers

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              “Active load control during rolling maneuvers” Metadata:

              • Title: ➤  Active load control during rolling maneuvers
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
              • Publish Date:
              • Publish Location: Springfield, VA - Hampton, Va

              “Active load control during rolling maneuvers” 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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                8A CFD study of tilt rotor flowfields

                By

                “A CFD study of tilt rotor flowfields” Metadata:

                • Title: ➤  A CFD study of tilt rotor flowfields
                • Author:
                • Language: English
                • Publisher: ➤  Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center - Stanford University, Dept. of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: Stanford, CA

                “A CFD study of tilt rotor flowfields” 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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                  9Determination of stores pointing error due to wing flexibility under flight load

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                  “Determination of stores pointing error due to wing flexibility under flight load” Metadata:

                  • Title: ➤  Determination of stores pointing error due to wing flexibility under flight load
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
                  • Publish Date:
                  • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                  “Determination of stores pointing error due to wing flexibility under flight load” 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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                    10Response of the alliance 1 proof-of-concept airplane under gust loads

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                    “Response of the alliance 1 proof-of-concept airplane under gust loads” Metadata:

                    • Title: ➤  Response of the alliance 1 proof-of-concept airplane under gust loads
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for Aerospace Information
                    • Publish Date:
                    • Publish Location: Hanover, MD - Hampton, Va

                    “Response of the alliance 1 proof-of-concept airplane under gust loads” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 2001
                    • 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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                      11An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data

                      By

                      “An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data” Metadata:

                      • Title: ➤  An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data
                      • Author:
                      • Language: English
                      • Publisher: ➤  Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Dryden Flight Research Center
                      • Publish Date:
                      • Publish Location: Edwards, Calif - Hanover, MD

                      “An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data” 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.

                      Online Borrowing:

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