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Source: The Open Library

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Search results from The Open Library

1In-flight transport performance optimization

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“In-flight transport performance optimization” Metadata:

  • Title: ➤  In-flight transport performance optimization
  • Author:
  • Language: English
  • Number of Pages: Median: 15
  • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Edwards, Calif

“In-flight transport performance optimization” 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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    2Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft

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    “Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft” Metadata:

    • Title: ➤  Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Lockheed-California Co. - For sale by the National Technical Information Service
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Burbank, Calif - Hampton, Va

    “Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1983
    • 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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      3Aileron controls for wind turbine applications

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      “Aileron controls for wind turbine applications” Metadata:

      • Title: ➤  Aileron controls for wind turbine applications
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
      • Publish Date:
      • Publish Location: [Cleveland, Ohio?]

      “Aileron controls for wind turbine applications” 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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        4Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration

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        “Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration” Metadata:

        • Title: ➤  Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration
        • Author:
        • Language: English
        • Number of Pages: Median: 36
        • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
        • Publish Date:
        • Publish Location: ➤  Washington, D.C - [Springfield, Va

        “Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration” 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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        5Theoretical study of the rolling response of aircraft to turbulent air

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        “Theoretical study of the rolling response of aircraft to turbulent air” Metadata:

        • Title: ➤  Theoretical study of the rolling response of aircraft to turbulent air
        • Author:
        • Language: English
        • Number of Pages: Median: 31
        • Publisher: H.M.S.O.
        • Publish Date:
        • Publish Location: London

        “Theoretical study of the rolling response of aircraft to turbulent air” Subjects and Themes:

        Edition Identifiers:

        • The Open Library ID: OL5568371M
        • Online Computer Library Center (OCLC) ID: 6184103
        • Library of Congress Control Number (LCCN): 67074993

        Access and General Info:

        • First Year Published: 1966
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        6Summary of NASA/DOE aileron-control development program for wind turbines

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        “Summary of NASA/DOE aileron-control development program for wind turbines” Metadata:

        • Title: ➤  Summary of NASA/DOE aileron-control development program for wind turbines
        • Author:
        • Language: English
        • Publisher: ➤  U.S. Dept. of Energy, Conservation and Renewable Energy, Wind/Ocean Technology Division - For sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: ➤  [Washington, DC] - [Springfield, Va

        “Summary of NASA/DOE aileron-control development program for wind turbines” 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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          7Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6

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          “Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6” Metadata:

          • Title: ➤  Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6
          • Author:
          • Language: English
          • Number of Pages: Median: 103
          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
          • Publish Date:
          • Publish Location: [Washington] - Springfield, Va

          “Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1978
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          8Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration

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          “Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration” Metadata:

          • Title: ➤  Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration
          • Author:
          • Language: English
          • Number of Pages: Median: 36
          • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
          • Publish Date:
          • Publish Location: ➤  Washington, D.C - [Springfield, Va

          “Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration” 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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          9Aileron controls for wind turbine applications

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          “Aileron controls for wind turbine applications” Metadata:

          • Title: ➤  Aileron controls for wind turbine applications
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
          • Publish Date:
          • Publish Location: [Cleveland, Ohio?]

          “Aileron controls for wind turbine applications” 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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            10Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application

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            “Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application” Metadata:

            • Title: ➤  Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application
            • Author:
            • Language: English
            • Publisher: ➤  For sale by the National Technical Information Service - U.S. Dept. of Energy, Conservation and Renewable Energy, Wind/Ocean Technology Division
            • Publish Date:
            • Publish Location: ➤  Washington, D.C - [Springfield, Va

            “Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application” 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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              11Reynolds number effects on the performance of lateral control devices

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              “Reynolds number effects on the performance of lateral control devices” Metadata:

              • Title: ➤  Reynolds number effects on the performance of lateral control devices
              • 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

              “Reynolds number effects on the performance of lateral control devices” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 2000
              • 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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                12Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic, compressible flow

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                “Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic, compressible flow” Metadata:

                • Title: ➤  Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic, compressible flow
                • Author:
                • Number of Pages: Median: 21
                • Publisher: ➤  National Aeronautical Research Institute
                • Publish Date:
                • Publish Location: Amsterdam

                “Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic, compressible flow” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1954
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                13Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap

                By

                “Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap” Metadata:

                • Title: ➤  Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap
                • Author:
                • Language: English
                • Number of Pages: Median: 91
                • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautic and Space Administration
                • Publish Date:
                • Publish Location: Washington - Springfield, Va

                “Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1977
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Marketplaces

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                14Development of an advanced composite aileron for the L-1011 transport aircraft

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                “Development of an advanced composite aileron for the L-1011 transport aircraft” Metadata:

                • Title: ➤  Development of an advanced composite aileron for the L-1011 transport aircraft
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Admininstration, Scientific and Technical Information Branch
                • Publish Date:
                • Publish Location: [Washington, D.C.?]

                “Development of an advanced composite aileron for the L-1011 transport aircraft” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1982
                • 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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                  15Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds

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                  “Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds” Metadata:

                  • Title: ➤  Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 39
                  • Publisher: H.M.S.O.
                  • Publish Date:
                  • Publish Location: London

                  “Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1966
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Marketplaces

                  Find Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds at online marketplaces:


                  16Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed

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                  “Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed” Metadata:

                  • Title: ➤  Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed
                  • Author: ➤  
                  • Language: English
                  • Number of Pages: Median: 44
                  • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                  • Publish Date:
                  • Publish Location: Langley Field, VA

                  “Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1944
                  • Is Full Text Available: Yes
                  • Is The Book Public: Yes
                  • Access Status: Public

                  Online Access

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                    17Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron

                    By

                    “Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron” Metadata:

                    • Title: ➤  Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron
                    • Author: ➤  
                    • Language: English
                    • Number of Pages: Median: 24
                    • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                    • Publish Date:
                    • Publish Location: Langley Field, VA

                    “Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1945
                    • Is Full Text Available: Yes
                    • Is The Book Public: Yes
                    • Access Status: Public

                    Online Access

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                      18Analysis of available data on the effectiveness of ailerons without exposed overhang balance

                      By

                      “Analysis of available data on the effectiveness of ailerons without exposed overhang balance” Metadata:

                      • Title: ➤  Analysis of available data on the effectiveness of ailerons without exposed overhang balance
                      • Author: ➤  
                      • Language: English
                      • Number of Pages: Median: 46
                      • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                      • Publish Date:
                      • Publish Location: Langley Field, VA

                      “Analysis of available data on the effectiveness of ailerons without exposed overhang balance” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1944
                      • Is Full Text Available: Yes
                      • Is The Book Public: Yes
                      • Access Status: Public

                      Online Access

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                        19Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane

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                        “Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane” Metadata:

                        • Title: ➤  Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane
                        • Author: ➤  
                        • Language: English
                        • Number of Pages: Median: 20
                        • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                        • Publish Date:
                        • Publish Location: Langley Field, VA

                        “Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1944
                        • Is Full Text Available: Yes
                        • Is The Book Public: Yes
                        • Access Status: Public

                        Online Access

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                          20Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces

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                          “Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces” Metadata:

                          • Title: ➤  Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces
                          • Author: ➤  
                          • Language: English
                          • Number of Pages: Median: 56
                          • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                          • Publish Date:
                          • Publish Location: Langley Field, VA

                          “Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1945
                          • Is Full Text Available: Yes
                          • Is The Book Public: Yes
                          • Access Status: Public

                          Online Access

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                            21Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

                            By

                            “Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil” Metadata:

                            • Title: ➤  Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil
                            • Author: ➤  
                            • Language: English
                            • Number of Pages: Median: 76
                            • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                            • Publish Date:
                            • Publish Location: Langley Field, VA

                            “Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1945
                            • Is Full Text Available: Yes
                            • Is The Book Public: Yes
                            • Access Status: Public

                            Online Access

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                              22Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap

                              By

                              “Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap” Metadata:

                              • Title: ➤  Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap
                              • Author: ➤  
                              • Language: English
                              • Number of Pages: Median: 20
                              • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                              • Publish Date:
                              • Publish Location: Langley Field, VA

                              “Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1942
                              • Is Full Text Available: Yes
                              • Is The Book Public: Yes
                              • Access Status: Public

                              Online Access

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                                23Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance

                                By

                                “Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance” Metadata:

                                • Title: ➤  Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance
                                • Author: ➤  
                                • Language: English
                                • Number of Pages: Median: 58
                                • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                                • Publish Date:
                                • Publish Location: Langley Field, VA

                                “Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1945
                                • Is Full Text Available: Yes
                                • Is The Book Public: Yes
                                • Access Status: Public

                                Online Access

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                                  24Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls

                                  By

                                  “Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls” Metadata:

                                  • Title: ➤  Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls
                                  • Author: ➤  
                                  • Language: English
                                  • Number of Pages: Median: 36
                                  • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                                  • Publish Date:
                                  • Publish Location: Langley Field, VA

                                  “Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1945
                                  • Is Full Text Available: Yes
                                  • Is The Book Public: Yes
                                  • Access Status: Public

                                  Online Access

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                                    25Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed

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                                    “Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed” Metadata:

                                    • Title: ➤  Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed
                                    • Author: ➤  
                                    • Language: English
                                    • Number of Pages: Median: 16
                                    • Publisher: ➤  Langley Memorial Aeronautical Laboratory
                                    • Publish Date:
                                    • Publish Location: Langley Field, VA

                                    “Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1943
                                    • Is Full Text Available: Yes
                                    • Is The Book Public: Yes
                                    • Access Status: Public

                                    Online Access

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