Accession Number:

AD0766788

Title:

Development of Composite Joints in Graphite/Epoxy Laminates of Modulite 5206-II.

Descriptive Note:

Progress rept.,

Corporate Author:

NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIR VEHICLE TECHNOLOGY DEPT

Personal Author(s):

Report Date:

1973-06-22

Pagination or Media Count:

38.0

Abstract:

Efficient and reliable joints and fastening systems for advanced fiber reinforced composites were studied. Optimum processing conditions were established for manufacturing a graphite composite wing for the BQM-34E serial target and also to determine the effect of surface fiber orientation on joint strength. The strength of Modulite 5206-11 graphiteepoxy composite joint to metal adherend depended primarily on the characteristics of the adhesive. A FLEXIBLE ADHESIVE LOADS THE COMPOSITE UNIFORMLY AND THE STRENGTH OF THE JOINT WILL DEPEND ON INTERLAMINA SHEAR PROPERTIES OF THE COMPOSITE. Author, modified-PL

Subject Categories:

  • Couplers, Fasteners and Joints

Distribution Statement:

APPROVED FOR PUBLIC RELEASE