Accession Number:

AD0678501

Title:

DEVELOPMENT OF ADHESIVE-BONDED JOINTS FOR GLASS RESIN COMPOSITE SANDWICH STRUCTURES.

Descriptive Note:

Technical rept. 29 May 67-29 May 68,

Corporate Author:

UNITED AIRCRAFT CORP STRATFORD CONN SIKORSKY AIRCRAFT DIV

Personal Author(s):

• Lutters,Samuel F.
• Bonassar,Maron J.

Report Date:

1968-08-01

Pagination or Media Count:

62.0

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

Descriptors:

• *AIRFRAMES
• *BONDED JOINTS
• SANDWICH PANELS
• GLASS TEXTILES
• WOOD
• EPOXY RESINS
• MANUFACTURING
• IMPREGNATION
• ADHESION
• SHEAR STRESSES
• STRESSES
• TENSILE PROPERTIES
• COMPRESSIVE PROPERTIES
• BENDING
• REDUCTION OF AREA
• FAILURE(MECHANICS)

Subject Categories:

• Adhesives, Seals and Binders
• Laminates and Composite Materials

Distribution Statement:

APPROVED FOR PUBLIC RELEASE