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Source: The Open Library

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1Assessment of dual-point drag reduction for an executive-jet modified airfoil section

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“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Metadata:

  • Title: ➤  Assessment of dual-point drag reduction for an executive-jet modified airfoil section
  • Author:
  • Language: English
  • Number of Pages: Median: 114
  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from National Technical Information Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langly Research Center
  • Publish Date:
  • Publish Location: ➤  Hampton, Virginia - Springfield, VA - Hampton, Va - [Springfield, Va

“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” 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

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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    2The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel

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    “The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel” Metadata:

    • Title: ➤  The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel
    • Author:
    • Language: English
    • Number of Pages: Median: 186
    • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor - Available from the National Technical Information Service
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Springfield, VA - Moffett Field, Calif

    “The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1998
    • 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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      3Turbine blade-tip clearance excitation forces

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      “Turbine blade-tip clearance excitation forces” Metadata:

      • Title: ➤  Turbine blade-tip clearance excitation forces
      • Author:
      • Language: English
      • Number of Pages: Median: 91
      • Publisher: ➤  National Technical Information Service, distributor - Massachusetts Institute of Technology - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  Cambridge, Mass - Springfield, Va - [Washington, DC

      “Turbine blade-tip clearance excitation forces” 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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        4Validation of vortex-lattice method for loads on wings in lift-generated wakes

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        “Validation of vortex-lattice method for loads on wings in lift-generated wakes” Metadata:

        • Title: ➤  Validation of vortex-lattice method for loads on wings in lift-generated wakes
        • Author:
        • Language: English
        • Publisher: ➤  American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - Washington, DC

        “Validation of vortex-lattice method for loads on wings in lift-generated wakes” 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:

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          5Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation

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          “Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Metadata:

          • Title: ➤  Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
          • Author:
          • Language: English
          • Publisher: ➤  North Carolina State University, Dept. of Mechanical and Aerospace Engineering
          • Publish Date:
          • Publish Location: Raleigh, [N.C.]

          “Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1990
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Access

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            6Manipulation of micro scale particles in an optical trap using interferometry

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            “Manipulation of micro scale particles in an optical trap using interferometry” Metadata:

            • Title: ➤  Manipulation of micro scale particles in an optical trap using interferometry
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
            • Publish Date:
            • Publish Location: ➤  [Cleveland, Ohio] - Hanover, MD

            “Manipulation of micro scale particles in an optical trap using interferometry” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 2002
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

            Downloads Are Not Available:

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              7Expanded equations for torque and force on a cylindrical permanent magnet core in a large-gap magnetic suspension system

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              “Expanded equations for torque and force on a cylindrical permanent magnet core in a large-gap magnetic suspension system” Metadata:

              • Title: ➤  Expanded equations for torque and force on a cylindrical permanent magnet core in a large-gap magnetic suspension system
              • 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

              “Expanded equations for torque and force on a cylindrical permanent magnet core in a large-gap magnetic suspension system” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1997
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

              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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                8Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction

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                “Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction” Metadata:

                • Title: ➤  Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
                • Publish Date:
                • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

                “Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction” 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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                  9A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas

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                  “A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas” Metadata:

                  • Title: ➤  A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
                  • Publish Date:
                  • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                  “A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas” 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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                    10Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler

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                    “Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler” Metadata:

                    • Title: ➤  Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler
                    • Author:
                    • Number of Pages: Median: 112
                    • Publisher: Langley Research Center
                    • Publish Date:
                    • Publish Location: Hampton, Va

                    “Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1979
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

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                    11Bubble generation in a continuous liquid flow under gravity conditions

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                    “Bubble generation in a continuous liquid flow under gravity conditions” Metadata:

                    • Title: ➤  Bubble generation in a continuous liquid flow under gravity conditions
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
                    • Publish Date:
                    • Publish Location: ➤  Springfield, VA - [Cleveland, Ohio]

                    “Bubble generation in a continuous liquid flow under gravity conditions” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1999
                    • 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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                      12Force balance and substorm effects in the magnetotail

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                      “Force balance and substorm effects in the magnetotail” Metadata:

                      • Title: ➤  Force balance and substorm effects in the magnetotail
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                      • Publish Date:
                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                      “Force balance and substorm effects in the magnetotail” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1997
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

                      Online Access

                      Downloads Are Not Available:

                      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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