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Hybrid Repair of Primary Metallic Structures by Combining a Stress Optimised Cut-Out and Bonded Patches

https://doi.org/10.2139/ssrn.4855745
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Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1016/0022-5096(58)90018-8openalex-extracted
The propagation of fatigue cracks in sheet specimens
inferredcites →https://doi.org/10.1016/j.compositesb.2015.09.038openalex-extracted
Experimental and finite element studies of thin bonded and hybrid carbon fibre double lap joints used in aircraft structures
inferredcites →https://doi.org/10.1016/j.compositesb.2016.06.061openalex-extracted
Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures
inferredcites →https://doi.org/10.1016/j.compstruc.2005.12.004openalex-extracted
Applying a genetic algorithm to the optimization of composite patches
inferredcites →https://doi.org/10.1016/j.compstruct.2014.11.004openalex-extracted
Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures
inferredcites →https://doi.org/10.1016/j.compstruct.2016.01.078openalex-extracted
Static and fatigue testing bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy laminates used on aircraft structures
inferredcites →https://doi.org/10.1016/j.compstruct.2018.09.038openalex-extracted
Hybrid approaches for aircraft primary structure repairs
inferredcites →https://doi.org/10.1016/j.engfracmech.2007.10.011openalex-extracted
Effect of local cold working on the fatigue life of 7475-T7351 aluminium alloy hole specimens
inferredcites →https://doi.org/10.1016/j.ijadhadh.2018.10.001openalex-extracted
Proposed through-life management approaches for adhesively bonded repair of primary structures
inferredcites →https://doi.org/10.1016/s0143-7496(03)00102-7openalex-extracted
Durability of an off-optimum cured aluminium joint
inferredcites →https://doi.org/10.1080/00218464.2014.883315openalex-extracted
On the Certification of Bonded Repairs to Primary Composite Aircraft Components
inferredcites →https://doi.org/10.2514/1.24300openalex-extracted
Design of Optimized Patches to Reinforce Damaged Wings
inferredcites →https://doi.org/10.2514/1.35712openalex-extracted
Design and Modelling of Selective Reinforcements for Integral Aircraft Structures
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