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Tensile stress-rupture and creep characteristics of two glass-fabric-base plastic laminates Public Deposited

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https://ir.library.oregonstate.edu/concern/defaults/pv63g398v

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. Information reviewed and reaffirmed 1965. Original report issued June 1957.

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  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-06-13T22:32:51Z (GMT) No. of bitstreams: 1 FPL_1863ocr.pdf: 3941455 bytes, checksum: 96823dc22de94473257ad9da75d7b5f7 (MD5)
  • description.provenance : Made available in DSpace on 2006-06-13T22:32:52Z (GMT). No. of bitstreams: 1 FPL_1863ocr.pdf: 3941455 bytes, checksum: 96823dc22de94473257ad9da75d7b5f7 (MD5) Previous issue date: 1965
  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-04-26T18:54:22Z No. of bitstreams: 1 FPL_1863ocr.pdf: 3941455 bytes, checksum: 96823dc22de94473257ad9da75d7b5f7 (MD5)

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