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

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https://ir.library.oregonstate.edu/concern/defaults/bv73c412q

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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  • 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.
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  • Scanned at 600 DPI using a Cannon DR-9080C in TIF format. PDF generated through Capture Perfect using OmniPage 14 Pro for textual OCR.
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  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-04-17T17:12:00Z No. of bitstreams: 1 FPL_1823-Bocr.pdf: 2819823 bytes, checksum: fff2e35f8876011b7bd443293c51dd71 (MD5)
  • description.provenance : Made available in DSpace on 2006-06-12T16:24:41Z (GMT). No. of bitstreams: 1 FPL_1823-Bocr.pdf: 2819823 bytes, checksum: fff2e35f8876011b7bd443293c51dd71 (MD5) Previous issue date: 1962
  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-06-12T16:24:38Z (GMT) No. of bitstreams: 1 FPL_1823-Bocr.pdf: 2819823 bytes, checksum: fff2e35f8876011b7bd443293c51dd71 (MD5)

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