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Supplement to fatigue tests of glass-fabric-base laminates subjected to axial loading

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  • This report presents the results of fatigue tests of an epoxide laminate subjected to axial loading. Direct stress tests were made at 0°, 15°, 30°, and 45° to the warp direction. Stress was applied at a frequency of 900 cycles per minute at zero mean stress on both unnotched and notched specimens. The results of a few bearing tests at 0° loading are also included. Data from the individual tests, and S-N curves based on these data, are presented. The S-N curves indicate how fatigue properties are affected by factors such as direction of loading, stress concentrations, and wet conditions.
  • This report is one of a series issued in cooperation with the ANC-17 Panel on Plastics for Aircraft of the Departments of the Air Force, Navy, and Commerce.
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