Explore: Propeller Blades

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Source: The Open Library

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1Structural Tailoring of Advanced Turboprops (STAT)

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“Structural Tailoring of Advanced Turboprops (STAT)” Metadata:

  • Title: ➤  Structural Tailoring of Advanced Turboprops (STAT)
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio] - [Washington, DC]

“Structural Tailoring of Advanced Turboprops (STAT)” 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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    2Low-speed wind-tunnel tests of single- and counter-rotation propellers

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    “Low-speed wind-tunnel tests of single- and counter-rotation propellers” Metadata:

    • Title: ➤  Low-speed wind-tunnel tests of single- and counter-rotation propellers
    • Author:
    • Language: English
    • Number of Pages: Median: 43
    • Publisher: ➤  National Aeronautics and Space Administration Scientific and Technical Information Branch - For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
    • Publish Date:
    • Publish Location: ➤  Hampton, Va - [Springfield, Va - [s.l.] - [Washington, D.C.]

    “Low-speed wind-tunnel tests of single- and counter-rotation propellers” 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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    Downloads Are Not Available:

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      3Advanced turboprop aircraft flyover noise

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      “Advanced turboprop aircraft flyover noise” Metadata:

      • Title: ➤  Advanced turboprop aircraft flyover noise
      • Author:
      • Language: English
      • Number of Pages: Median: 33
      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  Hampton, Va - [Springfield, Va.?

      “Advanced turboprop aircraft flyover noise” 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:

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        4Acoustic and aerodynamic study of a pusher-propeller aircraft model

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        “Acoustic and aerodynamic study of a pusher-propeller aircraft model” Metadata:

        • Title: ➤  Acoustic and aerodynamic study of a pusher-propeller aircraft model
        • 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: ➤  Springfield, Va - [Washington, D.C.]

        “Acoustic and aerodynamic study of a pusher-propeller aircraft model” 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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          5An unsteady lifting surface method for single rotation propellers

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          “An unsteady lifting surface method for single rotation propellers” Metadata:

          • Title: ➤  An unsteady lifting surface method for single rotation propellers
          • Author:
          • Number of Pages: Median: 53
          • Publisher: Lewis Research Center
          • Publish Date:
          • Publish Location: Cleveland, Ohio

          “An unsteady lifting surface method for single rotation propellers” 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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          6Crossflow and unsteady boundary-layer effects on rotating blades

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          “Crossflow and unsteady boundary-layer effects on rotating blades” Metadata:

          • Title: ➤  Crossflow and unsteady boundary-layer effects on rotating blades
          • Author:
          • Number of Pages: Median: 15
          • Publisher: ➤  American Institute of Aeronautics and Astronautics
          • Publish Date:
          • Publish Location: New York

          “Crossflow and unsteady boundary-layer effects on rotating blades” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1970
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          7Measurement of dynamic blade loadings for marine propellers

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          “Measurement of dynamic blade loadings for marine propellers” Metadata:

          • Title: ➤  Measurement of dynamic blade loadings for marine propellers
          • Author:
          • Publisher: ➤  Dept. of Aerospace Science and Engineering, University of Toronto
          • Publish Date:
          • Publish Location: [Downsview, Ont.]

          “Measurement of dynamic blade loadings for marine propellers” 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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          8Effect 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

          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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            9Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A

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            “Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A” Metadata:

            • Title: ➤  Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
            • Publish Date:
            • Publish Location: [Cleveland, Ohio

            “Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A” 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

            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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              10Design and establishment of an experimental facility to perform comparative studies of airfoil sections in rotating and rectilinear flight frames

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              “Design and establishment of an experimental facility to perform comparative studies of airfoil sections in rotating and rectilinear flight frames” Metadata:

              • Title: ➤  Design and establishment of an experimental facility to perform comparative studies of airfoil sections in rotating and rectilinear flight frames
              • Author:
              • Number of Pages: Median: 188
              • Publisher: ➤  Department of Aerospace Science and Engineering
              • Publish Date:
              • Publish Location: [Downsview, Ont.]

              “Design and establishment of an experimental facility to perform comparative studies of airfoil sections in rotating and rectilinear flight frames” 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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              11Near-field computations of propeller blade thickness noise

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              “Near-field computations of propeller blade thickness noise” Metadata:

              • Title: ➤  Near-field computations of propeller blade thickness noise
              • Author:
              • Number of Pages: Median: 24
              • Publisher: ➤  United Aircraft Corporation, Research Dept
              • Publish Date:
              • Publish Location: East Hartford, Conn

              “Near-field computations of propeller blade thickness noise” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1956
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              12Propeller noise caused by blade thickness

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              “Propeller noise caused by blade thickness” Metadata:

              • Title: ➤  Propeller noise caused by blade thickness
              • Author:
              • Number of Pages: Median: 18
              • Publisher: ➤  United Aircraft Corporation, Research Dept
              • Publish Date:
              • Publish Location: East Hartford, Conn

              “Propeller noise caused by blade thickness” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1956
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              13A review of propeller noise prediction methodology 1919-1994

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              “A review of propeller noise prediction methodology 1919-1994” Metadata:

              • Title: ➤  A review of propeller noise prediction methodology 1919-1994
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: [Springfield, Va - Hampton, Va

              “A review of propeller noise prediction methodology 1919-1994” 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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                14Optical measurement of propeller blade deflections

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                “Optical measurement of propeller blade deflections” Metadata:

                • Title: ➤  Optical measurement of propeller blade deflections
                • Author:
                • Language: English
                • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                • Publish Date:
                • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

                “Optical measurement of propeller blade deflections” 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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                  15Dynamic response and stability of a composite prop-fan model

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                  “Dynamic response and stability of a composite prop-fan model” Metadata:

                  • Title: ➤  Dynamic response and stability of a composite prop-fan model
                  • Author:
                  • Language: English
                  • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Lewis Research Center
                  • Publish Date:
                  • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va

                  “Dynamic response and stability of a composite prop-fan model” 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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                    16Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack

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                    “Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack” Metadata:

                    • Title: ➤  Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack
                    • Author:
                    • Language: English
                    • Publisher: Lewis Research Center
                    • Publish Date:
                    • Publish Location: Cleveland, Ohio

                    “Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack” 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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                      17Unsteady blade pressures on a propfan: predicted and measured compressibility effects

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                      “Unsteady blade pressures on a propfan: predicted and measured compressibility effects” Metadata:

                      • Title: ➤  Unsteady blade pressures on a propfan: predicted and measured compressibility effects
                      • Author:
                      • Publisher: ➤  American Institute of Aeronautics and Astronautics
                      • Publish Date:
                      • Publish Location: Washington, D. C

                      “Unsteady blade pressures on a propfan: predicted and measured compressibility effects” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1992
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

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                      Find Unsteady blade pressures on a propfan: predicted and measured compressibility effects at online marketplaces:


                      18Benefits of blade sweep for advanced turboprops

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                      “Benefits of blade sweep for advanced turboprops” Metadata:

                      • Title: ➤  Benefits of blade sweep for advanced turboprops
                      • Author:
                      • Number of Pages: Median: 11
                      • Publisher: AIAA
                      • Publish Date:
                      • Publish Location: New York

                      “Benefits of blade sweep for advanced turboprops” 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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                      19Unsteady potential flow past a propeller blade section

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                      “Unsteady potential flow past a propeller blade section” Metadata:

                      • Title: ➤  Unsteady potential flow past a propeller blade section
                      • Author:
                      • Number of Pages: Median: 25
                      • Publisher: Langley Research Center
                      • Publish Date:
                      • Publish Location: Hampton, Va

                      “Unsteady potential flow past a propeller blade section” 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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                      20Experimental classical flutter results of a composite advanced turboprop model

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                      “Experimental classical flutter results of a composite advanced turboprop model” Metadata:

                      • Title: ➤  Experimental classical flutter results of a composite advanced turboprop model
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
                      • Publish Date:
                      • Publish Location: ➤  [Springfield, Va - Cleveland, Ohio

                      “Experimental classical flutter results of a composite advanced turboprop model” 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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                        21An integrated optimum design approach for high speed prop rotors

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                        “An integrated optimum design approach for high speed prop rotors” Metadata:

                        • Title: ➤  An integrated optimum design approach for high speed prop rotors
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                        • Publish Date:
                        • Publish Location: ➤  [Washington, D.C - Springfield, Va

                        “An integrated optimum design approach for high speed prop rotors” 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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                          22Effect 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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                            23Unsteady potential flow past a propeller blade section

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                            “Unsteady potential flow past a propeller blade section” Metadata:

                            • Title: ➤  Unsteady potential flow past a propeller blade section
                            • Author:
                            • Language: English
                            • Number of Pages: Median: 25
                            • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
                            • Publish Date:
                            • Publish Location: ➤  Washington, D.C - [Springfield, Va

                            “Unsteady potential flow past a propeller blade section” 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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                              24Pressure distributions on the blade sections of the NACA 10-(3)(066)-033 propeller under operating conditions

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                              “Pressure distributions on the blade sections of the NACA 10-(3)(066)-033 propeller under operating conditions” Metadata:

                              • Title: ➤  Pressure distributions on the blade sections of the NACA 10-(3)(066)-033 propeller under operating conditions
                              • Author:
                              • Number of Pages: Median: 166
                              • Publisher: NACA
                              • Publish Date:
                              • Publish Location: Washington

                              “Pressure distributions on the blade sections of the NACA 10-(3)(066)-033 propeller under operating conditions” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1950
                              • 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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