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Hybrid approaches for aircraft primary structure repairs
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1016/0022-5096(58)90018-8openalex-snapshot
The propagation of fatigue cracks in sheet specimens
inferredcites →https://doi.org/10.1016/b978-008042699-0/50007-3openalex-snapshot
Fatigue Testing of Generic Bonded Joints
inferredcites →https://doi.org/10.1016/j.compositesa.2007.08.016openalex-snapshot
Review of z-pinned composite laminates
inferredcites →https://doi.org/10.1016/j.compositesa.2007.11.009openalex-snapshot
Improving performance of GFRP/aluminum single lap joints using bolted/co-cured hybrid method
inferredcites →https://doi.org/10.1016/j.compositesa.2010.03.006openalex-snapshot
Bonded repairs for carbon/BMI composite at high operating temperatures
inferredcites →https://doi.org/10.1016/j.compositesb.2006.03.006openalex-snapshot
Progressive failure modeling of woven fabric composite materials using multicontinuum theory
inferredcites →https://doi.org/10.1016/j.compositesb.2011.07.014openalex-snapshot
Battle damage repair of a helicopter composite main rotor blade
inferredcites →https://doi.org/10.1016/j.compositesb.2013.04.050openalex-snapshot
Damage monitoring and analysis of composite laminates with an open hole and adhesively bonded repairs using digital image correlation
inferredcites →https://doi.org/10.1016/j.compositesb.2015.09.038openalex-snapshot
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-snapshot
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.compscitech.2005.11.039openalex-snapshot
Properties and failure mechanisms of pinned composite lap joints in monotonic and cyclic tension
inferredcites →https://doi.org/10.1016/j.compstruc.2005.12.004openalex-snapshot
Applying a genetic algorithm to the optimization of composite patches
inferredcites →https://doi.org/10.1016/j.compstruct.2004.04.016openalex-snapshot
Load transfer in hybrid (bonded/bolted) composite single-lap joints
inferredcites →https://doi.org/10.1016/j.compstruct.2004.11.002openalex-snapshot
Quasi-static strength and fatigue life of hybrid (bonded/bolted) composite single-lap joints
inferredcites →https://doi.org/10.1016/j.compstruct.2006.04.013openalex-snapshot
Failure of carbon composite-to-aluminum joints with combined mechanical fastening and adhesive bonding
inferredcites →https://doi.org/10.1016/j.compstruct.2008.06.003openalex-snapshot
Analysis of bolted–bonded composite single-lap joints under combined in-plane and transverse loading
inferredcites →https://doi.org/10.1016/j.compstruct.2012.07.028openalex-snapshot
Analysis of adhesively bonded repairs in composites: Damage detection and prognosis
inferredcites →https://doi.org/10.1016/j.compstruct.2014.11.004openalex-snapshot
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-snapshot
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.2017.01.075openalex-snapshot
On the USAF ‘risk of failure’ approach and its applicability to composite repairs to metal airframes
inferredcites →https://doi.org/10.1016/j.ijadhadh.2004.11.007openalex-snapshot
Theoretical and experimental research into optimal edge taper of bonded repair patches subject to fatigue loadings
inferredcites →https://doi.org/10.1016/j.ijadhadh.2012.03.004openalex-snapshot
Development of a proof test for through-life monitoring of bond integrity in adhesively bonded repairs to aircraft structure
inferredcites →https://doi.org/10.1016/j.ijadhadh.2015.10.008openalex-snapshot
Advances in the proof test for certification of bonded repairs – Increasing the Technology Readiness Level
inferredcites →https://doi.org/10.1016/j.ijadhadh.2018.10.001openalex-snapshot
Proposed through-life management approaches for adhesively bonded repair of primary structures
inferredcites →https://doi.org/10.1017/s0001924000003778openalex-snapshot
Aspects of battle damage repair of helicopter structures
inferredcites →https://doi.org/10.1017/s0001924000044006openalex-snapshot
Concept and conduct of proof test of F-111 production aircraft
inferredcites →https://doi.org/10.1080/00218464.2014.883315openalex-snapshot
On the Certification of Bonded Repairs to Primary Composite Aircraft Components
inferredcites →https://doi.org/10.1080/14484846.2008.11464570openalex-snapshot
Optimum shapes for minimising bond stress in scarf repairs
inferredcites →https://doi.org/10.1115/1.2788984openalex-snapshot
A Multicontinuum Approach to Structural Analysis of Linear Viscoelastic Composite Materials
inferredcites →https://doi.org/10.2514/1.24300openalex-snapshot
Design of Optimized Patches to Reinforce Damaged Wings
inferredcites →https://doi.org/10.2514/1.24452openalex-snapshot
Analytical Two-Dimensional Model of a Hybrid (Bolted/Bonded) Single-Lap Joint
inferredcites →https://doi.org/10.2514/1.35712openalex-snapshot
Design and Modelling of Selective Reinforcements for Integral Aircraft Structures
inferredcites →https://doi.org/10.2514/6.2014-1534openalex-snapshot
Delamination Arrest by Multiple Fasteners in Bonded Composite Structures
inferredcites →https://doi.org/10.3390/ma9050374openalex-snapshot
Fatigue Damage Monitoring of a Composite Step Lap Joint Using Distributed Optical Fibre Sensors
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
inferred← citeshttps://doi.org/10.2139/ssrn.4855745openalex-extracted
Hybrid Repair of Primary Metallic Structures by Combining a Stress Optimised Cut-Out and Bonded Patches
inferred← citeshttps://doi.org/10.1007/s10409-019-00841-6openalex-snapshot
Study on establishment of standardized load spectrum on bogie frames of high-speed trains
inferred← citeshttps://doi.org/10.1007/s10853-026-13540-yopenalex-snapshot
History of the development of FeNiMnAl(Cr) multiprincipal component alloys
inferred← citeshttps://doi.org/10.1016/j.compositesa.2023.107479openalex-snapshot
Superior interfacial toughening of hybrid metal-composite structural joints using 3D printed pins
inferred← citeshttps://doi.org/10.1016/j.compstruct.2022.116021openalex-snapshot
A detailed study on the damage evolution and failure assessment of single-lap hybrid joints in CFRP laminates under tensile loading
inferred← citeshttps://doi.org/10.1016/j.compstruct.2024.118102openalex-snapshot
An experimental and parametrical study on repair of cracked titanium airframe structures with single-side bonded carbon fiber-reinforced polymer prepreg patches
inferred← citeshttps://doi.org/10.1016/j.enganabound.2025.106116openalex-snapshot
Fatigue analysis of crack propagation in structures with bonded composite repairs
inferred← citeshttps://doi.org/10.1016/j.engfailanal.2020.104664openalex-snapshot
Full-field strain distribution and failure characteristics of CFRP-repaired steel structures
inferred← citeshttps://doi.org/10.1016/j.engfailanal.2026.110574openalex-snapshot
The influence of localized repair techniques on the indentation performance of delaminated glass-fiber/epoxy laminates
inferred← citeshttps://doi.org/10.1016/j.ijadhadh.2025.103962openalex-snapshot
Hybrid repair of primary metallic structures by combining a stress optimised cut-out and bonded patches
inferred← citeshttps://doi.org/10.1016/j.ijfatigue.2025.109033openalex-snapshot
Experimental analysis of static and fatigue performance of hybrid double-lap joints in thin primary metallic aircraft structures
inferred← citeshttps://doi.org/10.1016/j.ijfatigue.2025.109177openalex-snapshot
Fatigue damage monitoring of hybrid step-lap joints in thick primary metallic aircraft structures using distributed optical fibre sensors
inferred← citeshttps://doi.org/10.1016/j.ijmecsci.2021.106344openalex-snapshot
Thermo-mechanical buckling of stepped circular bi-laminates
inferred← citeshttps://doi.org/10.1016/j.jcomc.2024.100554openalex-snapshot
Mechanical performance of hybrid double- and step-lap joints in primary metallic aircraft structures: An experimental and numerical approach
inferred← citeshttps://doi.org/10.1016/j.jcomc.2025.100567openalex-snapshot
Static and fatigue behaviour of hybrid step-lap joints in thick primary metallic aircraft structures
inferred← citeshttps://doi.org/10.1016/j.paerosci.2020.100641openalex-snapshot
The potential for structural simulation to augment full scale fatigue testing: A review
inferred← citeshttps://doi.org/10.1016/j.trpro.2021.02.059openalex-snapshot
Fatigue Strength of an Aircraft Wing Panel with a Repair Patch Based on the Filled Hole at Various Values of Interference Fit
inferred← citeshttps://doi.org/10.1080/00218464.2025.2519427openalex-snapshot
Experimental investigation on scarf repair of damaged composite honeycomb sandwich structures with adhesively bonded carbon fiber-reinforced prepreg patches
inferred← citeshttps://doi.org/10.1080/14658011.2021.1894696openalex-snapshot
Scarf patch repair of honeycomb sandwich composites and its simulation optimisation
inferred← citeshttps://doi.org/10.1177/09673911251333463openalex-snapshot
Injection repair for advanced aerospace composite materials
inferred← citeshttps://doi.org/10.21203/rs.3.rs-2994646/v1openalex-snapshot
Failure behavior of a notched plate repaired by a hybrid repair technique (Stop hole bonded composite
inferred← citeshttps://doi.org/10.21741/9781644902455-44openalex-snapshot
Numerical and experimental studies on the joint performance of fastened, bonded, and hybrid thin metal joints used in aircraft structures
inferred← citeshttps://doi.org/10.2514/1.c038187openalex-snapshot
Investigation on “Replacing Bolts with Rivets” in Composite Structures
inferred← citeshttps://doi.org/10.29019/enfoqueute.723openalex-snapshot
Ensayos experimentales y análisis numérico de la estructura del material compuesto alternativo para la reparación de superficies de vuelo en aeronaves
inferred← citeshttps://doi.org/10.3390/aerospace12060485openalex-snapshot
Research on Module Division of Commercial Aircraft Based on Analytic Hierarchy Process and Gray Fuzzy Comprehensive Evaluation
inferred← citeshttps://doi.org/10.3390/su15021159openalex-snapshot
Comparative Analysis of the Aviation Maintenance, Repair, and Overhaul (MRO) Industry in Northeast Asian Countries: A Suggestion for the Development of Korea’s MRO Industry
inferred← citeshttps://doi.org/10.7862/tiam.2022.3.6openalex-snapshot
Analysis of the airframe repair node
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