Fatigue of sandwich constructions for aircraft : Cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/ff3659049

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 2006-02-14T22:28:00Z No. of bitstreams: 1 FPL_1559-Focr.pdf: 6952287 bytes, checksum: a7e8353fa19f8f356369f5090ff2c9d0 (MD5)
  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-04-11T16:47:31Z (GMT) No. of bitstreams: 1 FPL_1559-Focr.pdf: 6952287 bytes, checksum: a7e8353fa19f8f356369f5090ff2c9d0 (MD5)
  • description.provenance : Made available in DSpace on 2006-04-11T16:47:32Z (GMT). No. of bitstreams: 1 FPL_1559-Focr.pdf: 6952287 bytes, checksum: a7e8353fa19f8f356369f5090ff2c9d0 (MD5) Previous issue date: 1948-12

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