DEVELOPMENT OF ADHESIVE-BONDED JOINTS FOR GLASS RESIN COMPOSITE SANDWICH STRUCTURES.
Technical rept. 29 May 67-29 May 68,
UNITED AIRCRAFT CORP STRATFORD CONN SIKORSKY AIRCRAFT DIV
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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
- Adhesives, Seals and Binders
- Laminates and Composite Materials