Design curves for the buckling of sandwich cylinders of finite length under uniform external lateral pressure Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/br86b756j

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 : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-07-11T20:15:34Z (GMT) No. of bitstreams: 1 FPL_1869ocr.pdf: 1674106 bytes, checksum: 85965779e6001388f035fc918eb5270b (MD5)
  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-04-28T19:40:07Z No. of bitstreams: 1 FPL_1869ocr.pdf: 1674106 bytes, checksum: 85965779e6001388f035fc918eb5270b (MD5)
  • description.provenance : Made available in DSpace on 2006-07-11T20:15:35Z (GMT). No. of bitstreams: 1 FPL_1869ocr.pdf: 1674106 bytes, checksum: 85965779e6001388f035fc918eb5270b (MD5) Previous issue date: 1959-05

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