EMPIRICAL DATE-DESIGN ALLOWABLES-BONDED ALUMINUM WING PANEL-USING FMS-0027-1C CORE AND FMS-0015-1 ADHESIVE-CONFIRMATION OF
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 13, 1962
- Accession Number
- AD0285152
Entities
People
- R.l. Vader
Organizations
- General Dynamics