Explore: Compressor Blades

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Source: The Open Library

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1NASA low-speed axial compressor for fundamental research

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“NASA low-speed axial compressor for fundamental research” Metadata:

  • Title: ➤  NASA low-speed axial compressor for fundamental research
  • Author:
  • Language: English
  • Number of Pages: Median: 11
  • Publisher: ➤  Lewis Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
  • Publish Date:
  • Publish Location: ➤  Cleveland, Ohio - [Washington, D.C.] - [Springfield, Va - [Washington, DC]

“NASA low-speed axial compressor for fundamental research” 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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    2Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading

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    “Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading” Metadata:

    • Title: ➤  Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
    • Publish Date:
    • Publish Location: [Cleveland, Ohio

    “Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading” 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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      3MATE program

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      “MATE program” Metadata:

      • Title: MATE program
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

      “MATE program” 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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        4Development of a fiber optic compressor blade sensor

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        “Development of a fiber optic compressor blade sensor” Metadata:

        • Title: ➤  Development of a fiber optic compressor blade sensor
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Washington, D.C - Springfield, Va

        “Development of a fiber optic compressor blade sensor” 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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          5Shot peening for Ti-6Al-4V alloy compressor blades

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          “Shot peening for Ti-6Al-4V alloy compressor blades” Metadata:

          • Title: ➤  Shot peening for Ti-6Al-4V alloy compressor blades
          • Author:
          • Publisher: Lewis Research Center
          • Publish Date:
          • Publish Location: Cleveland, Ohio

          “Shot peening for Ti-6Al-4V alloy compressor blades” 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 Marketplaces

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          6Advanced turboprop wing installation effects measured by unsteady blade pressure and noise

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          “Advanced turboprop wing installation effects measured by unsteady blade pressure and noise” Metadata:

          • Title: ➤  Advanced turboprop wing installation effects measured by unsteady blade pressure and noise
          • Author:
          • Language: English
          • Number of Pages: Median: 21
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

          “Advanced turboprop wing installation effects measured by unsteady blade pressure and noise” 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.

          Online Borrowing:

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            Find Advanced turboprop wing installation effects measured by unsteady blade pressure and noise at online marketplaces:


            7Secondary flow spanwise deviation model for the stators of NASA middle compressor stages

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            “Secondary flow spanwise deviation model for the stators of NASA middle compressor stages” Metadata:

            • Title: ➤  Secondary flow spanwise deviation model for the stators of NASA middle compressor stages
            • Author:
            • Language: English
            • Publisher: Lewis Research Center
            • Publish Date:
            • Publish Location: Cleveland, Ohio

            “Secondary flow spanwise deviation model for the stators of NASA middle compressor stages” 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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              8Investigation of blade vibration T55-L-11C compressor stages 1 and 2

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              “Investigation of blade vibration T55-L-11C compressor stages 1 and 2” Metadata:

              • Title: ➤  Investigation of blade vibration T55-L-11C compressor stages 1 and 2
              • Author:
              • Number of Pages: Median: 19
              • Publisher: ➤  Aeronautical Research Laboratories
              • Publish Date:
              • Publish Location: Melbourne, Victoria

              “Investigation of blade vibration T55-L-11C compressor stages 1 and 2” 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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              Find Investigation of blade vibration T55-L-11C compressor stages 1 and 2 at online marketplaces:


              9Experimental and numerical investigation of second-generation, controlled-diffusion, compressor blades in cascade

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              Book's cover

              “Experimental and numerical investigation of second-generation, controlled-diffusion, compressor blades in cascade” Metadata:

              • Title: ➤  Experimental and numerical investigation of second-generation, controlled-diffusion, compressor blades in cascade
              • Author:
              • Language: English
              • Number of Pages: Median: 75
              • Publisher: ➤  Available from National Technical Information Service - Naval Postgraduate School
              • Publish Date:
              • Publish Location: ➤  Monterey, Calif - Springfield, Va

              “Experimental and numerical investigation of second-generation, controlled-diffusion, compressor blades in cascade” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1997
              • Is Full Text Available: Yes
              • Is The Book Public: Yes
              • Access Status: Public

              Online Access

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                Wiki

                Source: Wikipedia

                Wikipedia Results

                Search Results from Wikipedia

                Axial compressor

                effectiveness of the compressor. In a rotor with blades moving say towards right. Let some blades receives flow at higher incidence, this blade will stop positively

                Compressor stall

                A compressor stall is a local disruption of the airflow in the compressor of a gas turbine or turbocharger. A stall that results in the complete disruption

                Compressor

                volumes is created by the rotating blades. Rotary vane compressors are, with piston compressors one of the oldest of compressor technologies. With suitable port

                Components of jet engines

                Axial compressors rely on spinning blades that have aerofoil sections, similar to aeroplane wings. As with aeroplane wings in some conditions the blades can

                Rolls-Royce Trent 1000

                Heavy Industries (intermediate compressor module), Mitsubishi Heavy Industries (combustor and low pressure turbine blades), Industria de Turbo Propulsores

                Compressor map

                A compressor map is a chart which shows the performance of a turbomachinery compressor. This type of compressor is used in gas turbine engines, for supercharging

                Centrifugal compressor

                Centrifugal compressors, sometimes called impeller compressors or radial compressors, are a sub-class of dynamic, axisymmetric, work-absorbing turbomachinery

                Air compressor

                velocity into a rise in pressure, and axial compressors, where rotor blades impart the kinetic energy and stator blades convert it to a rise in pressure. Due

                Junkers Jumo 004

                replacing compressor blades, (which suffered the most damage, usually from ingesting stones and such, later known as fodding) and turbine blades damaged

                Turbojet

                inlet guide vanes, a compressor, a combustion chamber, and a turbine (that drives the compressor). The compressed air from the compressor is heated by burning