Explore: Longitudinal Stability

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Source: The Open Library

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1Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring

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“Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” Metadata:

  • Title: ➤  Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
  • Author:
  • Language: English
  • Number of Pages: Median: 65
  • Publisher: ➤  National Technical Information Service, distributor - NASA, Dryden Flight Research Center - National Aeronautics and Space Administration, Dryden Flight Research Center - Available from National Technical Information Service
  • Publish Date:
  • Publish Location: ➤  Edwards, Calif - Springfield, Va - [Springfield, Va

“Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” 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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    2Euler/Navier-Stokes flow computations on flexible configurations for stability analysis

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    “Euler/Navier-Stokes flow computations on flexible configurations for stability analysis” Metadata:

    • Title: ➤  Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics
    • Publish Date:
    • Publish Location: ➤  Springfield, Va - [Washington, D.C

    “Euler/Navier-Stokes flow computations on flexible configurations for stability analysis” 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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      3Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration

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      “Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” Metadata:

      • Title: ➤  Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - [Washington, DC

      “Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” 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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        4Reduction of Blade-Vortex Interaction (BVI) noise through X-force control

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        “Reduction of Blade-Vortex Interaction (BVI) noise through X-force control” Metadata:

        • Title: ➤  Reduction of Blade-Vortex Interaction (BVI) noise through X-force control
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
        • Publish Date:
        • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

        “Reduction of Blade-Vortex Interaction (BVI) noise through X-force control” 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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          5Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination

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          “Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination” Metadata:

          • Title: ➤  Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Washington, DC - Springfield, Va

          “Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination” 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

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            6Low-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

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              7Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing

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              “Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing” Metadata:

              • Title: ➤  Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing
              • Author:
              • Language: English
              • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Va - [Springfield, Va

              “Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing” 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:

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                8Modeling of longitudinal unsteady aerodynamics of a wing-tail combination

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                “Modeling of longitudinal unsteady aerodynamics of a wing-tail combination” Metadata:

                • Title: ➤  Modeling of longitudinal unsteady aerodynamics of a wing-tail combination
                • 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

                “Modeling of longitudinal unsteady aerodynamics of a wing-tail combination” 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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                  9Theoretical investigations of the dynamics of bodies entering the atmosphere

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                  “Theoretical investigations of the dynamics of bodies entering the atmosphere” Metadata:

                  • Title: ➤  Theoretical investigations of the dynamics of bodies entering the atmosphere
                  • Author:
                  • Publisher: Institute of Aerophysics
                  • Publish Date:
                  • Publish Location: [Downsview, Ont.]

                  “Theoretical investigations of the dynamics of bodies entering the atmosphere” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1962
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

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                  10Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility

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                  “Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility” Metadata:

                  • Title: ➤  Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 67
                  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
                  • Publish Date:
                  • Publish Location: [Washington, D.C.]

                  “Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility” 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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                      12Locally 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

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                      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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                        13Transonic 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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                          14Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit

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                          “Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit” Metadata:

                          • Title: ➤  Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit
                          • Author:
                          • Number of Pages: Median: 18
                          • Publisher: ➤  Institute for Aerospace Studies
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1960
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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