Explore: Semispan Models

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Source: The Open Library

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1Semi-span model testing in the National Transonic Facility

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“Semi-span model testing in the National Transonic Facility” Metadata:

  • Title: ➤  Semi-span model testing in the National Transonic Facility
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Washington, DC

“Semi-span model testing in the National Transonic Facility” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1993
  • 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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    22-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall

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    “2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:

    • Title: ➤  2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
    • Author:
    • Language: English
    • Number of Pages: Median: 559
    • Publisher: ➤  National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
    • Publish Date:
    • Publish Location: ➤  Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va

    “2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” 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

    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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      3Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil

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      “Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Metadata:

      • Title: ➤  Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
      • Author:
      • Language: English
      • Number of Pages: Median: 48
      • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center
      • Publish Date:
      • Publish Location: ➤  [Washington, D.C.] - Springfield, Va - Hampton, Va

      “Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” 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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        4Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions

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        “Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions” Metadata:

        • Title: ➤  Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions
        • Author:
        • Language: English
        • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, VA - [Springfield, Va

        “Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions” 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:

        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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          5Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

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          “Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Metadata:

          • Title: ➤  Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
          • 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

          “Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” 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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            6Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model

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            “Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model” Metadata:

            • Title: ➤  Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center ; a Springfield, VA
            • Publish Date:
            • Publish Location: Hampton, Va

            “Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model” 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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              Find Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model at online marketplaces:


              7Aeroservoelastic testing of free flying wind tunnel models

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              “Aeroservoelastic testing of free flying wind tunnel models” Metadata:

              • Title: ➤  Aeroservoelastic testing of free flying wind tunnel models
              • Author:
              • Language: English
              • Number of Pages: Median: 45
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Virginia

              “Aeroservoelastic testing of free flying wind tunnel models” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 2013
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              8NACA 0015 wing pressure and trailing vortex measurements

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              “NACA 0015 wing pressure and trailing vortex measurements” Metadata:

              • Title: ➤  NACA 0015 wing pressure and trailing vortex measurements
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service , distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
              • Publish Date:
              • Publish Location: ➤  [Springfield, Va - Washington, D.C

              “NACA 0015 wing pressure and trailing vortex measurements” 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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                Find NACA 0015 wing pressure and trailing vortex measurements at online marketplaces:


                9Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model

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                “Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model” Metadata:

                • Title: ➤  Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model
                • Author:
                • Language: English
                • Number of Pages: Median: 108
                • 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.]

                “Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing 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

                Online Access

                Downloads Are Not Available:

                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                Online Borrowing:

                  Online Marketplaces

                  Find Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model at online marketplaces:


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