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 moderate thickness Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/n009w593d

This report is one of a series issued in cooperation with Air Force-Navy-Civil Subcomittee on aircraft design criteria under the supervision of the Aircraft Committee of the Munitions Board. Information reviewed and reaffirmed 1958. Original dated December 1951.

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  • description.provenance : Approved for entry into archive by Linda Kathman(linda.kathman@oregonstate.edu) on 2006-04-11T16:28:59Z (GMT) No. of bitstreams: 1 FPL_1583-Docr.pdf: 3459710 bytes, checksum: 318f16ba614eac2d96bfa1241768aee4 (MD5)
  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-02-20T16:04:50Z No. of bitstreams: 1 FPL_1583-Docr.pdf: 3459710 bytes, checksum: 318f16ba614eac2d96bfa1241768aee4 (MD5)
  • description.provenance : Made available in DSpace on 2006-04-11T16:28:59Z (GMT). No. of bitstreams: 1 FPL_1583-Docr.pdf: 3459710 bytes, checksum: 318f16ba614eac2d96bfa1241768aee4 (MD5) Previous issue date: 1958

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