DEVELOPMENT OF ADHESIVE-BONDED JOINTS FOR GLASS RESIN COMPOSITE SANDWICH STRUCTURES.
Abstract
The structural efficiencies of fiberglass resin composite structures were established for various adhesive bonded joint designs. The program covered three separate phases; design, fabrication and static testing of sandwich panels to determine their ability to take shear, tension, bending, and compression loads. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1968
- Accession Number
- AD0678501
Entities
People
- Maron J. Bonassar
- Samuel F. Lutters
Organizations
- United Aircraft Corporation