Explore: Hole Geometry (mechanics)

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Source: The Open Library

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1Analytical modeling of pressure wall hole size and maximum tip-to-tip crack length for perforating normal and oblique orbital debris impacts

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“Analytical modeling of pressure wall hole size and maximum tip-to-tip crack length for perforating normal and oblique orbital debris impacts” Metadata:

  • Title: ➤  Analytical modeling of pressure wall hole size and maximum tip-to-tip crack length for perforating normal and oblique orbital debris impacts
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - Civil & Environmental Engineering Dept., University of Alabama in Huntsville
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - Huntsville, Ala - [Washington, DC

“Analytical modeling of pressure wall hole size and maximum tip-to-tip crack length for perforating normal and oblique orbital debris impacts” 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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    2Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

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    “Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control” Metadata:

    • Title: ➤  Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va - [Springfield, Va

    “Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control” 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.

    Online Borrowing:

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      3Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application

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      “Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application” Metadata:

      • Title: ➤  Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application
      • 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

      “Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 2001
      • 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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        4Micromechanics of compression failures in open hole composite laminates

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        “Micromechanics of compression failures in open hole composite laminates” Metadata:

        • Title: ➤  Micromechanics of compression failures in open hole composite laminates
        • Author:
        • Language: English
        • Number of Pages: Median: 206
        • Publisher: ➤  Mechanics and Materials Center, Texas A&M University - National Technical Information Service, distributor - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Washington, D.C - College Station, Tex

        “Micromechanics of compression failures in open hole composite laminates” 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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          5Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

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          “Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades” Metadata:

          • Title: ➤  Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
          • Publish Date:
          • Publish Location: ➤  [Washington, D.C - Springfield, Va

          “Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades” 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.

          Online Borrowing:

            Online Marketplaces

            Find Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades at online marketplaces:


            6Standard methods for open hole tension testing of textile composites

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            “Standard methods for open hole tension testing of textile composites” Metadata:

            • Title: ➤  Standard methods for open hole tension testing of textile composites
            • 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

            “Standard methods for open hole tension testing of textile composites” 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.

            Online Borrowing:

              Online Marketplaces

              Find Standard methods for open hole tension testing of textile composites at online marketplaces:


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