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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

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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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      3Lateral-directional eigenvector flying qualities guidelines for high performance aircraft

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      “Lateral-directional eigenvector flying qualities guidelines for high performance aircraft” Metadata:

      • Title: ➤  Lateral-directional eigenvector flying qualities guidelines for high performance aircraft
      • 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

      “Lateral-directional eigenvector flying qualities guidelines for high performance aircraft” 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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        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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          5Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)

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          “Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)” Metadata:

          • Title: ➤  Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)
          • Author:
          • Language: English
          • Number of Pages: Median: 32
          • 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

          “Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)” 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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            6A study of the effects of CL-coupling on the lateral stability of aircraft in atmospheric turbulence

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            “A study of the effects of CL-coupling on the lateral stability of aircraft in atmospheric turbulence” Metadata:

            • Title: ➤  A study of the effects of CL-coupling on the lateral stability of aircraft in atmospheric turbulence
            • Author:
            • Language: English
            • Number of Pages: Median: 33
            • Publisher: ➤  Dept. of Electrical Engineering, University of Toronto - Institute for Aerospace Studies
            • Publish Date:
            • Publish Location: ➤  [Toronto, Ont.] - [Downsview, Ont.]

            “A study of the effects of CL-coupling on the lateral stability of aircraft in atmospheric turbulence” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1967
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            7Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration

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            “Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration” Metadata:

            • Title: ➤  Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration
            • Author:
            • Language: English
            • Number of Pages: Median: 30
            • 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

            “Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration” 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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              8VORSTAB, a computer program for calculating lateral-directional stability derivatives with vortex flow effect

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              “VORSTAB, a computer program for calculating lateral-directional stability derivatives with vortex flow effect” Metadata:

              • Title: ➤  VORSTAB, a computer program for calculating lateral-directional stability derivatives with vortex flow effect
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: [Springfield, Va - Hampton, Va

              “VORSTAB, a computer program for calculating lateral-directional stability derivatives with vortex flow effect” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1985
              • 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 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 Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
                • Publish Date:
                • Publish Location: ➤  Hanover, MD - Springfield, VA - Hampton, Va

                “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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                  10Lateral 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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                    11Cg/stability map for the reference H cycle 3 supersonic transport concept along the high speed research baseline mission profile

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                    “Cg/stability map for the reference H cycle 3 supersonic transport concept along the high speed research baseline mission profile” Metadata:

                    • Title: ➤  Cg/stability map for the reference H cycle 3 supersonic transport concept along the high speed research baseline mission profile
                    • 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

                    “Cg/stability map for the reference H cycle 3 supersonic transport concept along the high speed research baseline mission profile” 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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                      12A note on the T-tail flutter

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                      “A note on the T-tail flutter” Metadata:

                      • Title: A note on the T-tail flutter
                      • Author:
                      • Number of Pages: Median: 15
                      • Publisher: Royal Aircraft Establishment
                      • Publish Date:
                      • Publish Location: [S.l.]

                      “A note on the T-tail flutter” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1971
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

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                      13Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft

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                      “Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft” Metadata:

                      • Title: ➤  Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft
                      • Author:
                      • Language: English
                      • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
                      • Publish Date:
                      • Publish Location: ➤  [Springfield, Va - Edwards, Calif

                      “Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft” 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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                        14Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept

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                        “Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” Metadata:

                        • Title: ➤  Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
                        • Publish Date:
                        • Publish Location: [Springfield, Va - MSFC, Ala

                        “Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” 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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                          15On the lateral instabilities of aircraft due to parametric excitation

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                          “On the lateral instabilities of aircraft due to parametric excitation” Metadata:

                          • Title: ➤  On the lateral instabilities of aircraft due to parametric excitation
                          • Author:
                          • Number of Pages: Median: 38
                          • Publisher: ➤  Institute for Aerospace Studies
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “On the lateral instabilities of aircraft due to parametric excitation” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1965
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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