Abstract
This paper presents the concluding results of the large area composite structure repair program in which five large panels were repaired and subjected to static tests. A description of the Northrop bonded-cocured scarf joint repair is given with a review of strength and durability test results. Application of this technique to the problem presented in each of five panels is discussed. Finally, the repair of a speedbrake damaged in service is described. Repairability of advanced composite structure is fully demonstrated.
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