Accession Number : AD0285152

Title :   EMPIRICAL DATE-DESIGN ALLOWABLES-BONDED ALUMINUM WING PANEL-USING FMS-0027-1C CORE AND FMS-0015-1 ADHESIVE-CONFIRMATION OF

Corporate Author : GENERAL DYNAMICS/POMONA CALIF

Personal Author(s) : VADER,R.L.

Report Date : 13 SEP 1962

Pagination or Media Count : 1

Abstract : Research was conducted to provide empirical data from tests conducted on a bonded Al panel containing 6.1 lb/cu ft 5052 Al core and thin (FMS- 0015-1) 422J adhesive. The ultimate load and mode of failure of each specimen were recorded. (Author)

Descriptors :   *AIRPLANE PANELS, *ALUMINUM ALLOYS, ADHESIVES, BONDING, FAILURE (MECHANICS), SHEAR STRESSES, TENSILE PROPERTIES

Distribution Statement : APPROVED FOR PUBLIC RELEASE