Explore: Directional Stability

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Source: The Open Library

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1Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack

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“Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack” Metadata:

  • Title: ➤  Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
  • Author:
  • Language: English
  • Number of Pages: Median: 35
  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center - National Technical Information Service, distributor]
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C] - [Springfield, Va - [Washington, D.C.]

“Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack” 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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    2X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data

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    “X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data” Metadata:

    • Title: ➤  X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
    • Author:
    • Language: English
    • Number of Pages: Median: 35
    • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center - National Aeronautics and Space Administration - National Technical Information Service, distributor]
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C] - Washington, D.C - [Springfield, Va - [Washington, D.C.]

    “X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data” 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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      3Hi-alpha forebody design

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      “Hi-alpha forebody design” Metadata:

      • Title: Hi-alpha forebody design
      • Author:
      • Language: English
      • Publisher: ➤  Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University - National Aeronautics and Space Administration - National Technical Information Service, distributor]
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - [Washington, DC - Blacksburg, VA

      “Hi-alpha forebody design” 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

      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 wind tunnel tests of two waverider configuration models

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        “Low-speed wind tunnel tests of two waverider configuration models” Metadata:

        • Title: ➤  Low-speed wind tunnel tests of two waverider configuration models
        • Author:
        • Language: English
        • Publisher: ➤  [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Washington, D.C - Springfield, Va

        “Low-speed wind tunnel tests of two waverider configuration models” 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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          5Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates

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          “Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates” Metadata:

          • Title: ➤  Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Edwards, Calif - Springfield, VA

          “Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates” 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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            6Controls design with crossfeeds for hovering rotcract using quantitative feedback theory

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            “Controls design with crossfeeds for hovering rotcract using quantitative feedback theory” Metadata:

            • Title: ➤  Controls design with crossfeeds for hovering rotcract using quantitative feedback theory
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  Springfield, Va - [Washington, DC

            “Controls design with crossfeeds for hovering rotcract using quantitative feedback theory” 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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              7Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory

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              “Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory” Metadata:

              • Title: ➤  Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  Springfield, Va - [Washington, DC

              “Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory” 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 computational examination of directional stability for smooth and chined forebodies at High-α

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                “A computational examination of directional stability for smooth and chined forebodies at High-α” Metadata:

                • Title: ➤  A computational examination of directional stability for smooth and chined forebodies at High-α
                • 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: ➤  [Springfield, Va - [Washington, DC]

                “A computational examination of directional stability for smooth and chined forebodies at High-α” 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

                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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                  9Lateral stability analysis for X-29A drop model using system identification methodology

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                  “Lateral stability analysis for X-29A drop model using system identification methodology” Metadata:

                  • Title: ➤  Lateral stability analysis for X-29A drop model using system identification methodology
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 24
                  • 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, DC] - [Springfield, Va

                  “Lateral stability analysis for X-29A drop model using system identification methodology” 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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                    10Vehicle integration effects on hypersonic waveriders

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                    “Vehicle integration effects on hypersonic waveriders” Metadata:

                    • Title: ➤  Vehicle integration effects on hypersonic waveriders
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - [Washington, DC

                    “Vehicle integration effects on hypersonic waveriders” 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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                      11A computational examination of directional stability for smooth and chined forebodies at High-Ü

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                      “A computational examination of directional stability for smooth and chined forebodies at High-Ü” Metadata:

                      • Title: ➤  A computational examination of directional stability for smooth and chined forebodies at High-Ü
                      • 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, DC]

                      “A computational examination of directional stability for smooth and chined forebodies at High-Ü” 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

                      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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