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Source: The Open Library

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1XV-15 structural-acoustic data

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“XV-15 structural-acoustic data” Metadata:

  • Title: XV-15 structural-acoustic data
  • 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

“XV-15 structural-acoustic data” 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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    2Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover

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    “Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover” Metadata:

    • Title: ➤  Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover
    • Author:
    • Language: English
    • Number of Pages: Median: 142
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center - Ames Research Center
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Washington, D. C - Moffett Field, Calif

    “Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover” 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

    Online Access

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      3Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept

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      “Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” Metadata:

      • Title: ➤  Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
      • Author:
      • Language: English
      • Number of Pages: Median: 36
      • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
      • Publish Date:
      • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, D.C.]

      “Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” 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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        4Analysis of small-scale rotor hover performance data

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        “Analysis of small-scale rotor hover performance data” Metadata:

        • Title: ➤  Analysis of small-scale rotor hover performance data
        • Author:
        • Language: English
        • Number of Pages: Median: 24
        • 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

        “Analysis of small-scale rotor hover performance data” 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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          5Aeroelastic stability of a full-scale hingeless rotor

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          “Aeroelastic stability of a full-scale hingeless rotor” Metadata:

          • Title: ➤  Aeroelastic stability of a full-scale hingeless rotor
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

          “Aeroelastic stability of a full-scale hingeless rotor” 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:

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            6Development of time response criteria for rotorcraft at hover and low speed

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            “Development of time response criteria for rotorcraft at hover and low speed” Metadata:

            • Title: ➤  Development of time response criteria for rotorcraft at hover and low speed
            • Author:
            • Number of Pages: Median: 213
            • Publisher: ➤  American Institute of Aeronautics and Astronautics
            • Publish Date:
            • Publish Location: New York N. Y

            “Development of time response criteria for rotorcraft at hover and low speed” 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

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            7Solution method for a hovering helicopter rotor using the Euler equations

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            “Solution method for a hovering helicopter rotor using the Euler equations” Metadata:

            • Title: ➤  Solution method for a hovering helicopter rotor using the Euler equations
            • Author:
            • Number of Pages: Median: 12
            • Publisher: ➤  American Institute of Aeronautics and Astronautics
            • Publish Date:
            • Publish Location: New York

            “Solution method for a hovering helicopter rotor using the Euler equations” 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

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            8Experimental and analytical studies of a model helicopter rotor in hover

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            “Experimental and analytical studies of a model helicopter rotor in hover” Metadata:

            • Title: ➤  Experimental and analytical studies of a model helicopter rotor in hover
            • Author:
            • Number of Pages: Median: 58
            • Publisher: Ames Research Center
            • Publish Date:
            • Publish Location: Moffett Field, Calif

            “Experimental and analytical studies of a model helicopter rotor in hover” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1981
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            9Free wake analysis of hover performance using a new influence coefficient method

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            “Free wake analysis of hover performance using a new influence coefficient method” Metadata:

            • Title: ➤  Free wake analysis of hover performance using a new influence coefficient method
            • Author:
            • Number of Pages: Median: 93
            • Publisher: Ames Research Center
            • Publish Date:
            • Publish Location: Moffett Field, Ca

            “Free wake analysis of hover performance using a new influence coefficient method” 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

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            103-D wake measurements near a hovering rotor for determining profile and induced drag

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            “3-D wake measurements near a hovering rotor for determining profile and induced drag” Metadata:

            • Title: ➤  3-D wake measurements near a hovering rotor for determining profile and induced drag
            • Author:
            • Number of Pages: Median: 65
            • Publisher: ➤  US Army Aviation and Troop Command, Aeroflightdynamics Directorate
            • Publish Date:
            • Publish Location: Moffett Field, Calif

            “3-D wake measurements near a hovering rotor for determining profile and induced drag” 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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            11Description of the U.S. Army small-scale 2-meter rotor test system

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            “Description of the U.S. Army small-scale 2-meter rotor test system” Metadata:

            • Title: ➤  Description of the U.S. Army small-scale 2-meter rotor test system
            • Author:
            • Number of Pages: Median: 57
            • Publisher: Langley Research Center
            • Publish Date:
            • Publish Location: Hampton, Va

            “Description of the U.S. Army small-scale 2-meter rotor test system” 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

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            12Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor

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            “Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor” Metadata:

            • Title: ➤  Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
            • Publish Date:
            • Publish Location: [Washington, DC]

            “Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor” 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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              13Preliminary investigation of motion requirements for the simulation of helicopter hover tasks

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              “Preliminary investigation of motion requirements for the simulation of helicopter hover tasks” Metadata:

              • Title: ➤  Preliminary investigation of motion requirements for the simulation of helicopter hover tasks
              • Author:
              • Number of Pages: Median: 29
              • Publisher: Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Va

              “Preliminary investigation of motion requirements for the simulation of helicopter hover tasks” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1980
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              14Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft

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              “Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft” Metadata:

              • Title: ➤  Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft
              • Author:
              • Language: English
              • Number of Pages: Median: 59
              • 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, D.C - Springfield, Va

              “Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft” 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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                15Performance and pressure data from a small model tilt-rotor in hover

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                “Performance and pressure data from a small model tilt-rotor in hover” Metadata:

                • Title: ➤  Performance and pressure data from a small model tilt-rotor in hover
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                • Publish Date:
                • Publish Location: ➤  [Springfield, Va - Moffett Field, CA

                “Performance and pressure data from a small model tilt-rotor in hover” 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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                  16The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover

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                  “The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover” Metadata:

                  • Title: ➤  The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 56
                  • 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, D.C - [Springfield, Va

                  “The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover” 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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                    17Wide speed range turboshaft study

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                    “Wide speed range turboshaft study” Metadata:

                    • Title: ➤  Wide speed range turboshaft study
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                    • Publish Date:
                    • Publish Location: ➤  [Washington, D.C - Springfield, Va

                    “Wide speed range turboshaft study” 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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                      18Navier-Stokes calculations of the flowfield of a helicopter rotor in hover

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                      “Navier-Stokes calculations of the flowfield of a helicopter rotor in hover” Metadata:

                      • Title: ➤  Navier-Stokes calculations of the flowfield of a helicopter rotor in hover
                      • Author:
                      • Publisher: ➤  American Institute of Aeronautics and Astronautics
                      • Publish Date:
                      • Publish Location: Washington

                      “Navier-Stokes calculations of the flowfield of a helicopter rotor in hover” 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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                      19Navier-Stokes calculations for the vortex wake of a rotor in hover

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                      “Navier-Stokes calculations for the vortex wake of a rotor in hover” Metadata:

                      • Title: ➤  Navier-Stokes calculations for the vortex wake of a rotor in hover
                      • Author:
                      • Publisher: ➤  American Institute of Aeronautics and Astronautics
                      • Publish Date:
                      • Publish Location: New York

                      “Navier-Stokes calculations for the vortex wake of a rotor in hover” 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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                      20Design and evaluation of a cockpit display for hovering flight

                      By

                      “Design and evaluation of a cockpit display for hovering flight” Metadata:

                      • Title: ➤  Design and evaluation of a cockpit display for hovering flight
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                      • Publish Date:
                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                      “Design and evaluation of a cockpit display for hovering flight” 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

                      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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                        21Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades

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                        “Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades” Metadata:

                        • Title: ➤  Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
                        • Author:
                        • Language: English
                        • Publisher: ➤  US Army Aviation Systems Command, Aviation Research and Technology Activity - National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service, distributor
                        • Publish Date:
                        • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                        “Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades” 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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                          22Flow field around a hovering rotor

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                          “Flow field around a hovering rotor” Metadata:

                          • Title: ➤  Flow field around a hovering rotor
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                          “Flow field around a hovering rotor” 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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                            23A two dimensional study of rotor/airfoil interaction in hover

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                            “A two dimensional study of rotor/airfoil interaction in hover” Metadata:

                            • Title: ➤  A two dimensional study of rotor/airfoil interaction in hover
                            • Author:
                            • Language: English
                            • Publisher: ➤  Stanford University - National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                            • Publish Date:
                            • Publish Location: ➤  Moffett Field, Calif - [Palo Alto, Calif.] - [Springfield, Va

                            “A two dimensional study of rotor/airfoil interaction in hover” 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

                            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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                              24Rotor vortex filaments

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                              “Rotor vortex filaments” Metadata:

                              • Title: Rotor vortex filaments
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                              • Publish Date:
                              • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                              “Rotor vortex filaments” 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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                                25Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover

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                                “Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover” Metadata:

                                • Title: ➤  Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
                                • Publish Date:
                                • Publish Location: [Cleveland, Ohio]

                                “Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover” 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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                                  26Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover

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                                  “Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover” Metadata:

                                  • Title: ➤  Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                                  • Publish Date:
                                  • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                  “Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover” 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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                                    27Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft

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                                    “Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft” Metadata:

                                    • Title: ➤  Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                                    • Publish Date:
                                    • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                    “Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft” 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

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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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