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Supplement to torsion of sandwich panels of trapezoidal, triangular, and rectangular cross sections : derivation of differential equation and its application to rectangular panels with loads applied at corners Public Deposited

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This report is one of a series issued in cooperation with the ANC-23 panel on composite construction for flight vehicles of the departments of the Air Force, Navy, and Commerce.

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  • Torsion of sandwich panels of trapezoidal, triangular, and rectangular cross sections : derivation of differential equation and its application to rectangular panels with loads applied at corners
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  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-07-11T21:01:44Z (GMT) No. of bitstreams: 1 FPL_1874-Aocr.pdf: 1697144 bytes, checksum: c205e3830f1c618917f45622b4f35685 (MD5)
  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-04-28T22:13:03Z No. of bitstreams: 1 FPL_1874-Aocr.pdf: 1697144 bytes, checksum: c205e3830f1c618917f45622b4f35685 (MD5)
  • description.provenance : Made available in DSpace on 2006-07-11T21:01:45Z (GMT). No. of bitstreams: 1 FPL_1874-Aocr.pdf: 1697144 bytes, checksum: c205e3830f1c618917f45622b4f35685 (MD5) Previous issue date: 1960-11

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