Explore: High Aspect Ratio

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Source: The Open Library

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1Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

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“Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber” Metadata:

  • Title: ➤  Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Washington, DC] - [Springfield, Va

“Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber” 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

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    2Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber

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    “Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber” Metadata:

    • Title: ➤  Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - [Washington, DC]

    “Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber” 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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      3The effect of cooling passage aspect ratio on curvature heat transfer enhancement

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      “The effect of cooling passage aspect ratio on curvature heat transfer enhancement” Metadata:

      • Title: ➤  The effect of cooling passage aspect ratio on curvature heat transfer enhancement
      • Author:
      • Language: English
      • Number of Pages: Median: 16
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
      • Publish Date:
      • Publish Location: ➤  [Cleveland, Ohio] - [Springfield, Va

      “The effect of cooling passage aspect ratio on curvature heat transfer enhancement” 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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        4Electrically heated tube investigation of cooling channel geometry effects

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        “Electrically heated tube investigation of cooling channel geometry effects” Metadata:

        • Title: ➤  Electrically heated tube investigation of cooling channel geometry effects
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Washington, DC] - [Springfield, Va

        “Electrically heated tube investigation of cooling channel geometry effects” 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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          5Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles

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          “Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles” Metadata:

          • Title: ➤  Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

          “Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles” 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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            6A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center

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            “A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center” Metadata:

            • Title: ➤  A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
            • Author:
            • Language: English
            • Number of Pages: Median: 28
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - [Washington, D.C.?]

            “A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center” 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.

            Online Borrowing:

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              Find A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center at online marketplaces:



              Wiki

              Source: Wikipedia

              Wikipedia Results

              Search Results from Wikipedia

              Aspect ratio (aeronautics)

              Thus, a long, narrow wing has a high aspect ratio, whereas a short, wide wing has a low aspect ratio. Aspect ratio and other features of the planform

              Aspect ratio

              The aspect ratio of a geometric shape is the ratio of its sizes in different dimensions. For example, the aspect ratio of a rectangle is the ratio of its

              Aspect ratio (image)

              The aspect ratio of an image is the ratio of its width to its height. It is expressed as two numbers separated by a colon, in the format width:height

              Display aspect ratio

              The display aspect ratio (DAR) is the aspect ratio of a display device and so the proportional relationship between the physical width and the height of

              Pixel aspect ratio

              A pixel aspect ratio (PAR) is a mathematical ratio that describes how the width of a pixel in a digital image compares to the height of that pixel. Most

              Fullscreen (aspect ratio)

              screen) refers to the 4:3 (1.33:1) aspect ratio of early standard television screens and computer monitors. Widescreen ratios started to become more popular

              Bird wing

              these types. These types of wings are elliptical wings, high-speed wings, high aspect ratio wings and soaring wings with slots. Elliptical wings are

              16:9 aspect ratio

              aspect ratio with a width of 16 units and height of 9 units. Once seen as an "exotic" aspect ratio, since 2009, it has become the most common aspect ratio

              21:9 aspect ratio

              of this screen aspect ratio is a constant display height when displaying other content with a lesser aspect ratio. The 64:27 aspect ratio of "21:9" is an

              Dry etching

              wet etch to do anisotropic etching (removal of material) to create high aspect ratio structures (e.g. deep holes or capacitor trenches). The dry etching