Reminds me of the Forest Products Labs. Their research into plywood manufacturing and applications goes back to 1910. You can download the test reports from their library, which is on-line now.
The aero types in the crowd may find it interesting to note that many techniques of structural analysis of "sandwich panels" were studied thoroughly by the Forest Products Labs. These days, the typical aircraft sandwich panel is faced with aluminum or fiberglass, and the core is usually a honeycomb of flame-retardant-soaked nylon (or more aluminum) but the original idea seemed to be plywood facings with corrugated paper core. You can always find the FPL in the references sections of books like Bruhn or ESDU, and in the airframe design manuals used by the OEM's, and, of course, the ANC-18 wood design manual that is still "acceptable data" to the FAA.
STF