Explore: Ground Effect (aerodynamics)

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Source: The Open Library

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1XV-15 structural-acoustic data

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“XV-15 structural-acoustic data” Metadata:

  • Title: XV-15 structural-acoustic data
  • 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

“XV-15 structural-acoustic data” 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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    2Application of two procedures for dual-point design of transonic airfoils

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    “Application of two procedures for dual-point design of transonic airfoils” Metadata:

    • Title: ➤  Application of two procedures for dual-point design of transonic airfoils
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  Hampton - Hampton, Va - [Springfield, Va

    “Application of two procedures for dual-point design of transonic airfoils” 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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      3Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration

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      “Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration” Metadata:

      • Title: ➤  Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
      • Author:
      • Language: English
      • Number of Pages: Median: 28
      • Publisher: ➤  Langley Research Center - 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: ➤  Springfield, Va - Hampton, Va - [Washington, D.C.]

      “Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration” 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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        4Advanced method for computing the flow around wings with rear separation and ground effect

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        “Advanced method for computing the flow around wings with rear separation and ground effect” Metadata:

        • Title: ➤  Advanced method for computing the flow around wings with rear separation and ground effect
        • Author:
        • Number of Pages: Median: 62
        • Publisher: ➤  DFVLR Institut fur Theoretische Stromungsmechanik
        • Publish Date:
        • Publish Location: Gottingen

        “Advanced method for computing the flow around wings with rear separation and ground effect” 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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        5An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet

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        “An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet” Metadata:

        • Title: ➤  An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

        “An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet” 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:

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          6A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect

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          “A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect” Metadata:

          • Title: ➤  A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect
          • Author:
          • Number of Pages: Median: 207
          • Publisher: ➤  Dept. of Aerospace Science and Engineering
          • Publish Date:
          • Publish Location: [Downsview, Ont.]

          “A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect” 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

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          7Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets

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          “Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets” Metadata:

          • Title: ➤  Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets
          • Author:
          • Language: English
          • Number of Pages: Median: 21
          • 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: ➤  Springfield, Va - [Washington, D.C.]

          “Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets” 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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            83D visualization of unsteady 2D airplane wake vortices

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            “3D visualization of unsteady 2D airplane wake vortices” Metadata:

            • Title: ➤  3D visualization of unsteady 2D airplane wake vortices
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
            • Publish Date:
            • Publish Location: [Springfield, Va - Hampton, VA

            “3D visualization of unsteady 2D airplane wake vortices” 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:

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              9Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel

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              “Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel” Metadata:

              • Title: ➤  Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel
              • 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

              “Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel” 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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                10Propulsion/airframe interference for ducted propfan engines with ground effect

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                “Propulsion/airframe interference for ducted propfan engines with ground effect” Metadata:

                • Title: ➤  Propulsion/airframe interference for ducted propfan engines with ground effect
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                • Publish Date:
                • Publish Location: ➤  Springfield, Va - [Washington, DC

                “Propulsion/airframe interference for ducted propfan engines with ground effect” 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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                  11A two dimensional study of rotor/airfoil interaction in hover

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                  “A two dimensional study of rotor/airfoil interaction in hover” Metadata:

                  • Title: ➤  A two dimensional study of rotor/airfoil interaction in hover
                  • Author:
                  • Language: English
                  • Publisher: ➤  Stanford University - National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                  • Publish Date:
                  • Publish Location: ➤  Moffett Field, Calif - [Palo Alto, Calif.] - [Springfield, Va

                  “A two dimensional study of rotor/airfoil interaction in hover” 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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