Accession Number:

AD0285152

Title:

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

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/POMONA CALIF

Personal Author(s):

• VADER,R.L.

Report Date:

1962-09-13

Pagination or Media Count:

1.0

Abstract:

Research was conducted to provide empirical data from tests conducted on a bonded Al panel containing 6.1 lbcu 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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE