Kumar, AM and Singh, R (1997) 3D finite element modelling of a composite patch repair. In: 9th International Conference in Fracture (ICF9), Apr 01-05, 1997, Sydney, Australia.Full text not available from this repository.
Composite-patching on cracked/weak metallic aircraft structures improves structural integrity. A Boron Epoxy patch employed to repair a cracked Aluminum sheet is modeled employing 3D Finite Element Method (FEM). SIFs extracted using ''displacement extrapolation'' are used to measure the repair effectiveness. Two issues viz., patch taper and symmetry have been looked into.
|Item Type:||Conference Paper|
|Additional Information:||Copyright of this article belongs to Pergamon Press Ltd.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||15 Mar 2012 07:34|
|Last Modified:||15 Mar 2012 07:34|
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