Supplement to effects of shear deformation in the core of a flat rectangular sandwich panel : deflection under uniform load of sandwich panels having facings of unequal thickness Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/b8515s447

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. Information reviewed and reaffirmed 1962.

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  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-02-20T16:21:22Z No. of bitstreams: 1 FPL_1583-Cocr.pdf: 14904458 bytes, checksum: 001cb97f81ef7e0d5db2995accce4f1c (MD5)
  • description.provenance : Approved for entry into archive by Linda Kathman(linda.kathman@oregonstate.edu) on 2006-04-11T16:18:17Z (GMT) No. of bitstreams: 1 FPL_1583-Cocr.pdf: 14904458 bytes, checksum: 001cb97f81ef7e0d5db2995accce4f1c (MD5)
  • description.provenance : Made available in DSpace on 2006-04-11T16:18:18Z (GMT). No. of bitstreams: 1 FPL_1583-Cocr.pdf: 14904458 bytes, checksum: 001cb97f81ef7e0d5db2995accce4f1c (MD5) Previous issue date: 1962

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