Environmental evaluation of repairs to fuselage lap joints
1992; Elsevier BV; Volume: 21; Issue: 2 Linguagem: Inglês
10.1016/0263-8223(92)90047-g
ISSN1879-1085
AutoresL. Molent, N. Bridgford, D. Rees, R. Jones,
Tópico(s)Probabilistic and Robust Engineering Design
ResumoThis paper presents the results of a fatigue test programme undertaken to investigate repairs to multi-site damage in aircraft fuselage lap joints. It is demonstrated that a boron/epoxy composite doubler bonded over the joint should significantly increase the fatigue life of the structure and that environmental effects are negligible.
Referência(s)