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Source: The Open Library

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1Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

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“Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes” Metadata:

  • Title: ➤  Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes
  • Author:
  • Language: English
  • Number of Pages: Median: 77
  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service - Langley Research Center
  • Publish Date:
  • Publish Location: ➤  Washington, D.C - Hampton, Va - Springfield, Va

“Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes” 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

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    2Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle

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    “Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle” Metadata:

    • Title: ➤  Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle
    • Author:
    • Language: English
    • Number of Pages: Median: 107
    • Publisher: ➤  National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
    • Publish Date:
    • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

    “Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1993
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    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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      3Progress in multirate digital control system design

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      “Progress in multirate digital control system design” Metadata:

      • Title: ➤  Progress in multirate digital control system design
      • Author:
      • Language: English
      • Publisher: ➤  [Springfield, Va. : For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va

      “Progress in multirate digital control system design” 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:

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        4Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft

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        “Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft” Metadata:

        • Title: ➤  Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft
        • Author:
        • Language: English
        • Number of Pages: Median: 88
        • Publisher: ➤  Available from the National Technical Information Service - Langley Research Center - National Aeronautics and Space Administration, Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, Va - Springfield, VA

        “Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft” 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

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        5Effects of yaw and pitch motion on model attitude measurements

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        “Effects of yaw and pitch motion on model attitude measurements” Metadata:

        • Title: ➤  Effects of yaw and pitch motion on model attitude measurements
        • 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

        “Effects of yaw and pitch motion on model attitude measurements” 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

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          6The spinning of aircraft - a discussion of spin prediction techniques including a chronological bibliography (U)

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          “The spinning of aircraft - a discussion of spin prediction techniques including a chronological bibliography (U)” Metadata:

          • Title: ➤  The spinning of aircraft - a discussion of spin prediction techniques including a chronological bibliography (U)
          • Author:
          • Number of Pages: Median: 27
          • Publisher: ➤  Aeronautical Research Laboratory
          • Publish Date:
          • Publish Location: Melbourne, Victoria

          “The spinning of aircraft - a discussion of spin prediction techniques including a chronological bibliography (U)” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1988
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          7Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds

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          “Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Metadata:

          • Title: ➤  Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
          • Author:
          • Language: English
          • Number of Pages: Median: 51
          • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
          • Publish Date:
          • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

          “Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” 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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            8Formulas for propellers in yaw and charts of the side-force derivative

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            “Formulas for propellers in yaw and charts of the side-force derivative” Metadata:

            • Title: ➤  Formulas for propellers in yaw and charts of the side-force derivative
            • Author:
            • Number of Pages: Median: 15
            • Publisher: ➤  Langley Memorial Aeronautical Laboratory
            • Publish Date:
            • Publish Location: Langley Field, Va

            “Formulas for propellers in yaw and charts of the side-force derivative” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1943
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            9Propellers in yaw

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            “Propellers in yaw” Metadata:

            • Title: Propellers in yaw
            • Author:
            • Number of Pages: Median: 60
            • Publisher: ➤  Langley Memorial Aeronautical Laboratory
            • Publish Date:
            • Publish Location: Langley Field, Va

            “Propellers in yaw” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1943
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Marketplaces

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            10Proposal for a propeller side-force factor

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            “Proposal for a propeller side-force factor” Metadata:

            • Title: ➤  Proposal for a propeller side-force factor
            • Author:
            • Number of Pages: Median: 10
            • Publisher: ➤  Langley Memorial Aeronautical Laboratory
            • Publish Date:
            • Publish Location: Langley Field, Va

            “Proposal for a propeller side-force factor” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1943
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            11Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)

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            “Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)” Metadata:

            • Title: ➤  Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  Springfield, Va - [Washington, DC

            “Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)” 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:

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              12A parametric study of accelerations of an airplane due to a wake vortex system

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              “A parametric study of accelerations of an airplane due to a wake vortex system” Metadata:

              • Title: ➤  A parametric study of accelerations of an airplane due to a wake vortex system
              • 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

              “A parametric study of accelerations of an airplane due to a wake vortex system” 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

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                13Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles

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                “Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles” Metadata:

                • Title: ➤  Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
                • Author:
                • Language: English
                • Number of Pages: Median: 216
                • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
                • Publish Date:
                • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

                “Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles” 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

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                  14Experiments in aircraft roll-yaw control using forebody tangential blowing

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                  “Experiments in aircraft roll-yaw control using forebody tangential blowing” Metadata:

                  • Title: ➤  Experiments in aircraft roll-yaw control using forebody tangential blowing
                  • Author:
                  • Language: English
                  • Publisher: ➤  Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, Stanford University
                  • Publish Date:
                  • Publish Location: ➤  [Stanford, Calif.] - [Springfield, Va

                  “Experiments in aircraft roll-yaw control using forebody tangential blowing” 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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                    15Semicoarsening and implicit smoothers for the simulation of a flat plate at yaw

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                    “Semicoarsening and implicit smoothers for the simulation of a flat plate at yaw” Metadata:

                    • Title: ➤  Semicoarsening and implicit smoothers for the simulation of a flat plate at yaw
                    • Author:
                    • Language: English
                    • Publisher: ➤  ICASE, NASA Langley Research Center - Available from NASA Center for Aerospace Information
                    • Publish Date:
                    • Publish Location: Hampton, VA - Hanover, MD

                    “Semicoarsening and implicit smoothers for the simulation of a flat plate at yaw” 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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                      16Determination of shuttle orbiter center of gravity from flight measurements

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                      “Determination of shuttle orbiter center of gravity from flight measurements” Metadata:

                      • Title: ➤  Determination of shuttle orbiter center of gravity from flight measurements
                      • Author:
                      • Language: English
                      • Publisher: NASA Langley Research Center
                      • Publish Date:
                      • Publish Location: Hampton, Va

                      “Determination of shuttle orbiter center of gravity from flight measurements” 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:

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                        17The effect of pitch and yaw on the aerodynamic interference between two identical, unstaggered, axisymmetrical bodies whose centrelines are parallel and separated by 1.11 body diameters

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                        “The effect of pitch and yaw on the aerodynamic interference between two identical, unstaggered, axisymmetrical bodies whose centrelines are parallel and separated by 1.11 body diameters” Metadata:

                        • Title: ➤  The effect of pitch and yaw on the aerodynamic interference between two identical, unstaggered, axisymmetrical bodies whose centrelines are parallel and separated by 1.11 body diameters
                        • Author:
                        • Publisher: ➤  Cranfield Institute of Technology, College of Aeronautics
                        • Publish Date:
                        • Publish Location: Cranfield, Bedford, England

                        “The effect of pitch and yaw on the aerodynamic interference between two identical, unstaggered, axisymmetrical bodies whose centrelines are parallel and separated by 1.11 body diameters” 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

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                        18Evaluation of a circulation control tail boom for yaw control

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                        “Evaluation of a circulation control tail boom for yaw control” Metadata:

                        • Title: ➤  Evaluation of a circulation control tail boom for yaw control
                        • Author:
                        • Number of Pages: Median: 51
                        • Publisher: ➤  Applied Technology Laboratory, U.S. Army Research and Technology Laboratories
                        • Publish Date:
                        • Publish Location: Fort Eustis, Va

                        “Evaluation of a circulation control tail boom for yaw control” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1978
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

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