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Tensile and Tensile-Fatigue Properties of Transparent Enclosure Attachments for Aircraft.


AD020650

Publication Date 1953
Personal Author LIGGETT, R. D.; LATHAM, E.; STANSBURY, J.G.
Page Count 10
Abstract Fifteen types of edge attachments, eight for monolithic acrylic material and seven for laminated acrylic material were designed, fabricated and tested for tensile strength at room temperature and -65 degrees F, and in tensile-fatigue at room temperature. Thirteen of these types were designed using MIL-P-5425 acrylic material. (Author-PL).
Keywords
  • Transparent panels
  • Acrylic resins
  • Attachment
  • Laminates
  • Tensile properties
Source Agency
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
Corporate Authors Swedlow Plastics CO Los Angeles Calif
Document Type Technical Report
NTIS Issue Number 198107
Contract Number
  • AF33 038 22456
Tensile and Tensile-Fatigue Properties of Transparent Enclosure Attachments for Aircraft.
Tensile and Tensile-Fatigue Properties of Transparent Enclosure Attachments for Aircraft.
AD020650

  • Transparent panels
  • Acrylic resins
  • Attachment
  • Laminates
  • Tensile properties
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
  • AF33 038 22456
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