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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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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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    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

    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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      3Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops

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      “Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops” Metadata:

      • Title: ➤  Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops
      • Author:
      • Language: English
      • Number of Pages: Median: 63
      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - Hampton, Va - [Washington, D.C.]

      “Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops” 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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        4Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers

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        “Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers” Metadata:

        • Title: ➤  Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

        “Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers” 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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          5A numerical simulation of the inviscid flow through a counter-rotating propeller

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          “A numerical simulation of the inviscid flow through a counter-rotating propeller” Metadata:

          • Title: ➤  A numerical simulation of the inviscid flow through a counter-rotating propeller
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
          • Publish Date:
          • Publish Location: [Cleveland, Ohio

          “A numerical simulation of the inviscid flow through a counter-rotating propeller” 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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            6An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications

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            “An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications” Metadata:

            • Title: ➤  An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

            “An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications” 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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              7A 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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                8User's guide to PMESH - a grid-generation program for single-rotation and counterrotation advanced turboprops

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                “User's guide to PMESH - a grid-generation program for single-rotation and counterrotation advanced turboprops” Metadata:

                • Title: ➤  User's guide to PMESH - a grid-generation program for single-rotation and counterrotation advanced turboprops
                • Author:
                • Number of Pages: Median: 23
                • Publisher: Lewis Research Center
                • Publish Date:
                • Publish Location: Cleveland, Ohio

                “User's guide to PMESH - a grid-generation program for single-rotation and counterrotation advanced turboprops” 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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                9Comparison of advanced turboprop and conventional jet and propeller aircraft flyover noise annoyance

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                “Comparison of advanced turboprop and conventional jet and propeller aircraft flyover noise annoyance” Metadata:

                • Title: ➤  Comparison of advanced turboprop and conventional jet and propeller aircraft flyover noise annoyance
                • Author:
                • Language: English
                • Number of Pages: Median: 29
                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                • Publish Date:
                • Publish Location: Hampton, Va

                “Comparison of advanced turboprop and conventional jet and propeller aircraft flyover noise annoyance” 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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                  10Advanced 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.

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                    11Benefits 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

                    Online Marketplaces

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                    12Aerodynamic characteristics of a propeller-powered high-lift semispan wing

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                    “Aerodynamic characteristics of a propeller-powered high-lift semispan wing” Metadata:

                    • Title: ➤  Aerodynamic characteristics of a propeller-powered high-lift semispan wing
                    • Author:
                    • Number of Pages: Median: 67
                    • Publisher: Langley Research Center
                    • Publish Date:
                    • Publish Location: Hampton, Va

                    “Aerodynamic characteristics of a propeller-powered high-lift semispan wing” 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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                    13Effect of solidity and inclination on propeller-nacelle force coefficients

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                    “Effect of solidity and inclination on propeller-nacelle force coefficients” Metadata:

                    • Title: ➤  Effect of solidity and inclination on propeller-nacelle force coefficients
                    • Author:
                    • Number of Pages: Median: 20
                    • Publisher: Langley Research Center
                    • Publish Date:
                    • Publish Location: Hampton, Va

                    “Effect of solidity and inclination on propeller-nacelle force coefficients” 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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                    14Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise

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                    “Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise” Metadata:

                    • Title: ➤  Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise
                    • Author:
                    • Number of Pages: Median: 130
                    • Publisher: Lewis Research Center
                    • Publish Date:
                    • Publish Location: Cleveland, Ohio

                    “Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise” 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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                    Find Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise at online marketplaces:


                    15Experimental 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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                      16Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications

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                      “Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications” Metadata:

                      • Title: ➤  Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications
                      • 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

                      “Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications” 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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                        17GENENG

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                        “GENENG” Metadata:

                        • Title: GENENG
                        • Author:
                        • Number of Pages: Median: 31
                        • Publisher: ➤  Cranfield University, College of Aeronautics
                        • Publish Date:
                        • Publish Location: Cranfield, Bedford, England

                        “GENENG” 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

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