Explore: Counter Rotation

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Source: The Open Library

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1Measurements and modeling of flow structure in the wake of a low profile "wishbone" vortex generator

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“Measurements and modeling of flow structure in the wake of a low profile "wishbone" vortex generator” Metadata:

  • Title: ➤  Measurements and modeling of flow structure in the wake of a low profile "wishbone" vortex generator
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Washington, DC

“Measurements and modeling of flow structure in the wake of a low profile "wishbone" vortex generator” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1994
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    2Final technical report for aeroelastic analysis of counter rotation fans

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    “Final technical report for aeroelastic analysis of counter rotation fans” Metadata:

    • Title: ➤  Final technical report for aeroelastic analysis of counter rotation fans
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  Springfield, Va - [Washington, DC

    “Final technical report for aeroelastic analysis of counter rotation fans” 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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      3Acoustic test and analysis of a counterrotating prop-fan model

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      “Acoustic test and analysis of a counterrotating prop-fan model” Metadata:

      • Title: ➤  Acoustic test and analysis of a counterrotating prop-fan model
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
      • Publish Date:
      • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va

      “Acoustic test and analysis of a counterrotating prop-fan model” 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:

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        4Effect of angular inflow on the vibratory response of a counter-rotating propeller

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        “Effect of angular inflow on the vibratory response of a counter-rotating propeller” Metadata:

        • Title: ➤  Effect of angular inflow on the vibratory response of a counter-rotating propeller
        • Author:
        • Language: English
        • Publisher: ➤  NASA - For sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

        “Effect of angular inflow on the vibratory response of a counter-rotating propeller” 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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          5Numerical simulation of stability and stabiity control of high speed compressible rotating couette flow

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          “Numerical simulation of stability and stabiity control of high speed compressible rotating couette flow” Metadata:

          • Title: ➤  Numerical simulation of stability and stabiity control of high speed compressible rotating couette flow
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, DC

          “Numerical simulation of stability and stabiity control of high speed compressible rotating couette flow” 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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            6Some design philosophy for reducing the community noise of advanced counter-rotation propellers

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            “Some design philosophy for reducing the community noise of advanced counter-rotation propellers” Metadata:

            • Title: ➤  Some design philosophy for reducing the community noise of advanced counter-rotation propellers
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
            • Publish Date:
            • Publish Location: [Cleveland, Ohio

            “Some design philosophy for reducing the community noise of advanced counter-rotation propellers” 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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              7Optical measurement of unducted fan flutter

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              “Optical measurement of unducted fan flutter” Metadata:

              • Title: ➤  Optical measurement of unducted fan flutter
              • Author:
              • Language: English
              • Publisher: ➤  NASA - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  [Washington, DC] - [Springfield, Va

              “Optical measurement of unducted fan flutter” 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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                8Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions

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                “Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions” Metadata:

                • Title: ➤  Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
                • Publish Date:
                • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                “Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions” 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

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                  9Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)

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                  “Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)” Metadata:

                  • Title: ➤  Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 23
                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                  “Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)” 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:

                  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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                    10Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions

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                    “Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions” Metadata:

                    • Title: ➤  Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 23
                    • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

                    “Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions” 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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                      11Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance

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                      “Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance” Metadata:

                      • Title: ➤  Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center - For sale by the National Technical Information Service
                      • Publish Date:
                      • Publish Location: ➤  [Cleveland, Ohio] - [Springfield, Va

                      “Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance” 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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                        12Aerodynamic performance of a counter rotating prop-fan

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                        “Aerodynamic performance of a counter rotating prop-fan” Metadata:

                        • Title: ➤  Aerodynamic performance of a counter rotating prop-fan
                        • Author:
                        • Number of Pages: Median: 11
                        • Publisher: AIAA
                        • Publish Date:
                        • Publish Location: New York

                        “Aerodynamic performance of a counter rotating prop-fan” 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

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