Fatigue of sandwich constructions for aircraft : Fiberglas-laminate facing and paper honeycomb core sandwich material tested in shear Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/fq977z62s

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on aircraft design criteria under the supervision of the Aircraft Committee of the Munitions Board.

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  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-02-14T22:24:23Z No. of bitstreams: 1 FPL_1559-Gocr.pdf: 3851568 bytes, checksum: cb1a0d68f9c059a78ffd1af40c4226e4 (MD5)
  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-04-17T18:13:20Z (GMT) No. of bitstreams: 1 FPL_1559-Gocr.pdf: 3851568 bytes, checksum: cb1a0d68f9c059a78ffd1af40c4226e4 (MD5)
  • description.provenance : Made available in DSpace on 2006-04-17T18:13:21Z (GMT). No. of bitstreams: 1 FPL_1559-Gocr.pdf: 3851568 bytes, checksum: cb1a0d68f9c059a78ffd1af40c4226e4 (MD5) Previous issue date: 1949-02

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