A proposed composite repair methodology for primary structure
1989; Elsevier BV; Volume: 20; Issue: 5 Linguagem: Inglês
10.1016/0010-4361(89)90218-8
ISSN1878-7134
AutoresStephen R. Hall, M. D. Raizenne, Don Simpson,
Tópico(s)Mechanical Failure Analysis and Simulation
ResumoAbstract Advanced composite materials are used extensively in aircraft structures. A major problem with the use of these materials is that of structural repair. Composite structures require different repair techniques than do their metal counterparts. Presently, there is very little data available which permits composite structural repairs to be designed and evaluated. This paper details the steps that are required to generate an aircraft composite repair capability for primary structures.
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