The over-ply covering the bondline in scarf-repaired laminates can avoid direct exposure of
the adhesive to moisture environment which would decrease the properties of the adhesive …

The paper focused on the moisture absorption and hygrothermal degradation of composite
laminates repaired via double scarf method. Experimental works were carried out on double …

Both single-face vacuum bag curing (SVC) and double-face vacuum bag curing (DVC) can
be used in scarf repair of composite structures. But different curing conditions caused by the …

Experimental investigation on tensile behavior of hybrid plain woven fabric laminate
repaired by scarfing method was conducted in the paper. There were 3 types of specimens …

Tensile failure behavior of scarf repaired composite laminates was studied with non-linear
three dimensional finite element modeling. The finite element method (FEM) results are in …

Based on experimental study, damage propagation and ultimate strength of the scarf
repaired composite laminate were analyzed through a 3-D FEM (Finite Element Method) …

Adhesively bonded techniques have been widely used to joint or repair composite
components in aircraft structures, which are inevitably subjected to various environmental …

Composite structures are generally pressurized at both sides when repaired by the scarf
repair method. But single-face vacuum bag curing (SVC) may be used in some practical …

Scarf repair method which can get uniform stress distributions and smooth surfaces has
emerged as an adequate technique to repair damaged aerospace composite components …

Bonded scarf repairs are used in composite structures when high strength recovery is
desired or when there is a requirement for a smooth surface to satisfy aerodynamic …