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

http://ir.library.oregonstate.edu/concern/defaults/z890rz25w

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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  • 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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