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Analysis of skin-stringer debonding in composite panels through a two-way global-local method
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
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A concise interface constitutive law for analysis of delamination and splitting in composite materials and its application to scaled notched tensile specimens
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Yielding of steel sheets containing slits
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Interlaminar interface modelling for the prediction of delamination
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Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus
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The virtual crack closure technique for modeling interlaminar failure and delamination in advanced composite materials
inferredcites →https://doi.org/10.1016/j.compositesb.2012.02.010openalex-snapshot
Experimental and three-dimensional global-local finite element analysis of a composite component including degradation process at the interfaces
inferredcites →https://doi.org/10.1016/j.compositesb.2012.07.030openalex-snapshot
Failure analysis of composite multi-stringer panels using simplified models
inferredcites →https://doi.org/10.1016/j.compositesb.2014.11.007openalex-snapshot
A robust numerical approach for the simulation of skin–stringer debonding growth in stiffened composite panels under compression
inferredcites →https://doi.org/10.1016/j.compositesb.2016.03.058openalex-snapshot
Inter-laminar and intra-laminar damage evolution in composite panels with skin-stringer debonding under compression
inferredcites →https://doi.org/10.1016/j.compscitech.2008.07.017openalex-snapshot
Compression and post-buckling damage growth and collapse analysis of flat composite stiffened panels
inferredcites →https://doi.org/10.1016/j.compscitech.2008.12.015openalex-snapshot
Panel stiffener debonding analysis using a shell/3D modeling technique
inferredcites →https://doi.org/10.1016/j.compscitech.2015.04.010openalex-snapshot
On the use of global–local kinematic coupling approaches for delamination growth simulation in stiffened composite panels
inferredcites →https://doi.org/10.1016/j.compstruct.2007.01.012openalex-snapshot
Degradation investigation in a postbuckling composite stiffened fuselage panel
inferredcites →https://doi.org/10.1016/j.compstruct.2009.04.002openalex-snapshot
Multi-level experimental and numerical analysis of composite stiffener debonding. Part 2: Element and panel level
inferredcites →https://doi.org/10.1016/j.compstruct.2015.09.056openalex-snapshot
A two-way loose coupling procedure for investigating the buckling and damage behaviour of stiffened composite panels
inferredcites →https://doi.org/10.1016/j.compstruct.2017.02.011openalex-snapshot
Efficient progressive failure analysis of multi-stringer stiffened composite panels through a two-way loose coupling global-local approach
inferredcites →https://doi.org/10.1016/j.engfracmech.2006.03.006openalex-snapshot
Discrete cohesive zone model for mixed-mode fracture using finite element analysis
inferredcites →https://doi.org/10.1016/j.engfracmech.2006.08.025openalex-snapshot
An engineering solution for mesh size effects in the simulation of delamination using cohesive zone models
inferredcites →https://doi.org/10.1016/j.finel.2016.11.002openalex-snapshot
Simulation of delamination under impact using a global–local method in explicit dynamics
inferredcites →https://doi.org/10.1016/j.mechmat.2005.10.003openalex-snapshot
A damage model for the simulation of delamination in advanced composites under variable-mode loading
inferredcites →https://doi.org/10.1016/s0065-2156(08)70121-2openalex-snapshot
The Mathematical Theory of Equilibrium Cracks in Brittle Fracture
inferredcites →https://doi.org/10.1016/s0263-8223(01)00006-xopenalex-snapshot
Failure of thick-skinned stiffener runout sections loaded in uniaxial compression
inferredcites →https://doi.org/10.1016/s0263-8223(02)00110-1openalex-snapshot
The analysis of skin-to-stiffener debonding in composite aerospace structures
inferredcites →https://doi.org/10.1016/s0266-3538(00)00170-6openalex-snapshot
Modelling of splitting and delamination in notched cross-ply laminates
inferredcites →https://doi.org/10.1016/s0266-3538(00)00245-1openalex-snapshot
Simulation of delamination in fiber composites with a discrete cohesive failure model
inferredcites →https://doi.org/10.1142/s0219455407002253openalex-snapshot
EXPERIMENTS ON BUCKLING AND POSTBUCKLING OF THIN-WALLED CFRP STRUCTURES USING ADVANCED MEASUREMENT SYSTEMS
inferredcites →https://doi.org/10.1142/s0219455410003683openalex-snapshot
NUMERICAL TREATMENT OF DAMAGE PROPAGATION IN AXIALLY COMPRESSED COMPOSITE AIRFRAME PANELS
inferredcites →https://doi.org/10.1177/0021998305053504openalex-snapshot
Experimental Investigation of Progressive Damage and the Effect of Layup in Notched Tensile Tests
inferredcites →https://doi.org/10.1177/0021998305057432openalex-snapshot
Numerical Investigation of Progressive Damage and the Effect of Layup in Notched Tensile Tests
inferredcites →https://doi.org/10.2514/1.26910openalex-snapshot
Optimization Strategy for Minimizing Damage in Postbuckling Stiffened Panels
inferredcites →https://doi.org/10.2514/2.575openalex-snapshot
Global/Local Postbuckling Failure Analysis of Composite Stringer/Skin Panels
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
inferred← citeshttps://doi.org/10.1002/pc.70267openalex-snapshot
Applying the Stressing State Theory and Network‐Free Normalization Method Reveals the Failure Law of the Compression‐Loaded Stiffened Composite Panels With Stiffener Runout
inferred← citeshttps://doi.org/10.1007/978-3-030-11969-0_6openalex-snapshot
Post-buckling Progressive Failure Analysis of Composite Panels Using a Two-Way Global-Local Coupling Approach Including Intralaminar Failure and Debonding
inferred← citeshttps://doi.org/10.1007/978-981-33-4550-8_16openalex-snapshot
Modeling Fracture in Straight Fiber and Tow-Steered Fiber Laminated Composites—A Phase Field Approach
inferred← citeshttps://doi.org/10.1007/s10443-020-09850-2openalex-snapshot
Experimental and Numerical Study on Softened Inclusions Equivalent Method for Impacted Stiffened Panel Skin
inferred← citeshttps://doi.org/10.1007/s12289-019-01514-2openalex-snapshot
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inferred← citeshttps://doi.org/10.1016/j.compstruc.2021.106480openalex-snapshot
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inferred← citeshttps://doi.org/10.1016/j.compstruct.2018.10.083openalex-snapshot
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inferred← citeshttps://doi.org/10.1016/j.compstruct.2020.112532openalex-snapshot
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inferred← citeshttps://doi.org/10.1016/j.compstruct.2023.117233openalex-snapshot
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inferred← citeshttps://doi.org/10.1016/j.compstruct.2024.118276openalex-snapshot
Non-linear buckling analysis of delaminated hat-stringer panels using variational asymptotic method
inferred← citeshttps://doi.org/10.1016/j.compstruct.2024.118748openalex-snapshot
Lamb wave S0/A0 mode conversion for imaging the internal structure of composite panel
inferred← citeshttps://doi.org/10.1016/j.compstruct.2025.119245openalex-snapshot
Effect of delamination defects on buckling and growth characteristics in composite laminates
inferred← citeshttps://doi.org/10.1016/j.compstruct.2025.119838openalex-snapshot
Predicting compression strength and dynamic response of composite reinforced panel structure with debonding defect by numerical and experimental analysis
inferred← citeshttps://doi.org/10.1016/j.compstruct.2026.120299openalex-snapshot
Bistable laminates with stiffeners: Loss of bistability and stiffener debonding
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inferred← citeshttps://doi.org/10.1016/j.ijmecsci.2024.109737openalex-snapshot
Stress fields at skin-stringer junctions in composite aircraft fuselages
inferred← citeshttps://doi.org/10.1016/j.ijmecsci.2026.111902openalex-snapshot
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inferred← citeshttps://doi.org/10.1016/j.matpr.2021.05.290openalex-snapshot
Progressive delamination analysis of CFRP laminated plate under compressive loading
inferred← citeshttps://doi.org/10.1016/j.tws.2019.106231openalex-snapshot
Numerical FEA parametric analysis of CAI behaviour of CFRP stiffened panels
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Effects of fillers on the impact damage and compressive residual properties of single hat-stiffened composite panels
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Simulation of compression-induced buckling and debonding of stiffened composite panels based on cohesion free method
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Damage evolution in fuselage stiffened composite panels under asymmetrical bending loading conditions
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Influence of adhesive interface properties on the post-buckling response of composite I-stiffened panels with lateral support under axial compression
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A geometric modeling method for an integrally stiffened panel with three-dimensional woven composites
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Modeling test strain data reveal shear damage evolution characteristic of CFRP laminates
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Experimental and numerical investigation of damage evolution in carbon fiber reinforced polymer stiffened panel in post-buckling regime
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Post-buckling failure analysis of composite stiffened panels considering the mode III fracture
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A framework for physics-driven generation of feature data for strain-based damage detection in aerospace sandwich structures
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Stress Fields at Skin-Stringer Junctions in Modern Composite Passenger Aircraft Fuselages: A Layerwise Global-Local Analysis Approach
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High-Fidelity Reduced-Order Method for Postbuckling Analysis of Aeronautical Structures
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An Extended Dual Spring Modeling Approach for Static and Fatigue Failure Assessment of Composite Laminates with Stitching
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Research on the Manufacturing Quality of Co-Cured Hat-Stiffened Composite Structure
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