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Compressive buckling curves for sandwich cylinders having orthotropic facings Public Deposited

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https://ir.library.oregonstate.edu/concern/defaults/5138jk11f

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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  • Report no. 1876
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  • 2348039 bytes
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  • Scanned at 600 DPI using a Cannon DR-9080C in TIF format. PDF generated through Capture Perfect using OmniPage 14 Pro for textual OCR.
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  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-07-12T15:35:52Z (GMT) No. of bitstreams: 1 FPL_1876ocr.pdf: 2348039 bytes, checksum: 37fc73010689fd5f7959108b9d31a0e8 (MD5)
  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-04-28T22:34:27Z No. of bitstreams: 1 FPL_1876ocr.pdf: 2348039 bytes, checksum: 37fc73010689fd5f7959108b9d31a0e8 (MD5)
  • description.provenance : Made available in DSpace on 2006-07-12T15:35:53Z (GMT). No. of bitstreams: 1 FPL_1876ocr.pdf: 2348039 bytes, checksum: 37fc73010689fd5f7959108b9d31a0e8 (MD5) Previous issue date: 1960-07

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