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Source: The Open Library

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1A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor

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“A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor” Metadata:

  • Title: ➤  A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor
  • Author:
  • Language: English
  • Publisher: ➤  US Army Aviation Systems Command, Aviation Research and Technology Activity - NASA Ames Research Center
  • Publish Date:
  • Publish Location: Moffett Field, Calif

“A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor” 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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    2Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil

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    “Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Metadata:

    • Title: ➤  Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
    • Author:
    • Language: English
    • Number of Pages: Median: 48
    • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C.] - Springfield, Va - Hampton, Va

    “Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” 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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      3Design of supersonic transport flap systems for thrust recovery at subsonic speeds

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      “Design of supersonic transport flap systems for thrust recovery at subsonic speeds” Metadata:

      • Title: ➤  Design of supersonic transport flap systems for thrust recovery at subsonic speeds
      • 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

      “Design of supersonic transport flap systems for thrust recovery at subsonic speeds” 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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        4Low 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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          5Turbulence measurements on a flap-edge model

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          “Turbulence measurements on a flap-edge model” Metadata:

          • Title: ➤  Turbulence measurements on a flap-edge model
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, DC

          “Turbulence measurements on a flap-edge model” 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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            6Synthesis of individual rotor blade control system for gust alleviation

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            “Synthesis of individual rotor blade control system for gust alleviation” Metadata:

            • Title: ➤  Synthesis of individual rotor blade control system for gust alleviation
            • Author:
            • Language: English
            • Number of Pages: Median: 64
            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C - Springfield, Va

            “Synthesis of individual rotor blade control system for gust alleviation” 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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              7Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct

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              “Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct” Metadata:

              • Title: ➤  Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
              • 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

              “Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct” 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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                8Investigation of dynamic flight maneuvers with an iced tailplane

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                “Investigation of dynamic flight maneuvers with an iced tailplane” Metadata:

                • Title: ➤  Investigation of dynamic flight maneuvers with an iced tailplane
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
                • Publish Date:
                • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

                “Investigation of dynamic flight maneuvers with an iced tailplane” 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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                  9Application of higher harmonic control to hingeless rotor systems

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                  “Application of higher harmonic control to hingeless rotor systems” Metadata:

                  • Title: ➤  Application of higher harmonic control to hingeless rotor systems
                  • Author:
                  • Language: English
                  • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
                  • Publish Date:
                  • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                  “Application of higher harmonic control to hingeless rotor systems” 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.

                  Online Borrowing:

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