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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

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

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  • This report is one of a series issued in cooperation with Air Force-Navy-Civil Subcommittee 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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  • 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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