On the public citation graph
Effect of stiffener damage caused by low velocity impact on compressive buckling and failure modes of T-stiffened composite panels
0 signed · 73 inferred · view as graph
Inferred edges come from two machine sources: sweeps of open repository metadata (mostly SSRN and Zenodo), and a bulk OpenAlex citation snapshot. Every row below is labelled with the one it came from. Neither is a complete citation index — absence here is not evidence of absence.
Is this your work? Sign in with ORCID and put your name on the
claims that are yours.
Reference health. See whether every reference in this work resolves to a
known work and none has been retracted — and get a dated CiteStamped
badge you can embed.
What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1016/j.compositesa.2004.12.003openalex-snapshot
Stiffener debonding mechanisms in post-buckled CFRP aerospace panels
inferredcites →https://doi.org/10.1016/j.compositesa.2015.01.025openalex-snapshot
Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates
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.compositesb.2016.09.057openalex-snapshot
Low-velocity impact tests on carbon/epoxy composite laminates: A benchmark study
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.2008.10.025openalex-snapshot
Simulation of multiple delaminations in impacted cross-ply laminates using a finite element model based on cohesive interface elements
inferredcites →https://doi.org/10.1016/j.compscitech.2009.02.029openalex-snapshot
Experimental analysis of damage creation and permanent indentation on highly oriented plates
inferredcites →https://doi.org/10.1016/j.compscitech.2012.08.019openalex-snapshot
Low velocity impact modeling in composite laminates capturing permanent indentation
inferredcites →https://doi.org/10.1016/j.compstruct.2004.04.038openalex-snapshot
Influence of post-buckling behaviour of composite stiffened panels on the damage criticality
inferredcites →https://doi.org/10.1016/j.compstruct.2005.11.050openalex-snapshot
Buckling and postbuckling of stringer stiffened fibre composite curved panels – Tests and computations
inferredcites →https://doi.org/10.1016/j.compstruct.2011.11.011openalex-snapshot
Post-buckling analysis of composite plates containing embedded delaminations with arbitrary shape by using higher order shear deformation theory
inferredcites →https://doi.org/10.1016/j.compstruct.2012.03.039openalex-snapshot
Modelling damage evolution in composite laminates subjected to low velocity impact
inferredcites →https://doi.org/10.1016/j.compstruct.2012.06.005openalex-snapshot
Post-buckling behaviour of flat stiffened composite panels: Experiments vs. analysis
inferredcites →https://doi.org/10.1016/j.compstruct.2012.07.002openalex-snapshot
Composite damage model based on continuum damage mechanics and low velocity impact analysis of composite plates
inferredcites →https://doi.org/10.1016/j.compstruct.2012.08.054openalex-snapshot
Prediction of permanent indentation due to impact on laminated composites based on an elasto-plastic model incorporating fiber failure
inferredcites →https://doi.org/10.1016/j.compstruct.2013.02.027openalex-snapshot
Simulation of low velocity impact on composite laminates with progressive failure analysis
inferredcites →https://doi.org/10.1016/j.compstruct.2013.12.011openalex-snapshot
Low-velocity impact responses of the stiffened composite laminated plates based on the progressive failure model and the layerwise/solid-elements method
inferredcites →https://doi.org/10.1016/j.compstruct.2013.12.012openalex-snapshot
Experimental analysis of CFRP laminates subjected to compression after impact: The role of impact-induced cracks in failure
inferredcites →https://doi.org/10.1016/j.compstruct.2013.12.017openalex-snapshot
A non-linear shear damage model to reproduce permanent indentation caused by impacts in composite laminates
inferredcites →https://doi.org/10.1016/j.compstruct.2014.11.074openalex-snapshot
Experiment and analysis of hat-stringer-stiffened composite curved panels under axial compression
inferredcites →https://doi.org/10.1016/j.compstruct.2015.02.020openalex-snapshot
Edge impact modeling on stiffened composite structures
inferredcites →https://doi.org/10.1016/j.compstruct.2015.08.019openalex-snapshot
Experimental and numerical analysis for the post-buckling behavior of stiffened composite panels with impact damage
inferredcites →https://doi.org/10.1016/j.compstruct.2015.11.060openalex-snapshot
Experimental investigation on edge impact damage and Compression-After-Impact (CAI) behavior of stiffened composite panels
inferredcites →https://doi.org/10.1016/j.compstruct.2016.02.063openalex-snapshot
Micro–macro FE modeling of damage evolution in laminated composite plates subjected to low velocity impact
inferredcites →https://doi.org/10.1016/j.compstruct.2016.08.012openalex-snapshot
Effect of impact damage positions on the buckling and post-buckling behaviors of stiffened composite panel
inferredcites →https://doi.org/10.1016/j.compstruct.2016.09.099openalex-snapshot
Finite element analysis of dynamic progressive failure of plastic composite laminates under low velocity impact
inferredcites →https://doi.org/10.1016/j.compstruct.2016.12.004openalex-snapshot
Failure prediction of T-stiffened composite panels subjected to compression after edge impact
inferredcites →https://doi.org/10.1016/j.compstruct.2017.03.011openalex-snapshot
Compressive strength of composite laminates with delamination-induced interaction of panel and sublaminate buckling modes
inferredcites →https://doi.org/10.1016/s0263-8223(00)00146-xopenalex-snapshot
Post-buckling behavior of composite panels in the presence of unstable delaminations
inferredcites →https://doi.org/10.1016/s0263-8223(03)00116-8openalex-snapshot
Compression behavior of stitched stiffened panel with a clearly visible stiffener impact damage
inferredcites →https://doi.org/10.1016/s0263-8223(97)00117-7openalex-snapshot
Impact behaviour of stiffened CFRP sections
inferredcites →https://doi.org/10.1016/s0263-8223(98)00044-0openalex-snapshot
Postbuckling and failure of stiffened composite panels under axial compression
inferredcites →https://doi.org/10.1016/s1359-835x(00)00061-0openalex-snapshot
Delamination threshold loads for low velocity impact on composite laminates
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.4664121openalex-extracted
Effect of Embedded Shape Memory Alloy (Sma) on the Impact Behaviour of Stringer Stiffened Composite Plates
inferred← citeshttps://doi.org/10.1002/pc.26892openalex-snapshot
A novel methodology to research the residual compressive mechanical properties of composite stiffened panel after low velocity impact based on quantification damage simulation
inferred← citeshttps://doi.org/10.1007/978-3-030-68303-0_13openalex-snapshot
Study on Bearing Mechanism of Composite Stiffened Panel with Delamination Under Shear Load
inferred← citeshttps://doi.org/10.1007/978-981-95-3031-1_16openalex-snapshot
Numerical Simulation of Stiffener Impact Damage of T Stiffened Composite Panels
inferred← citeshttps://doi.org/10.1007/s10443-021-09891-1openalex-snapshot
Artificial Neural Network (ANN)-Based Residual Strength Prediction of Carbon Fibre Reinforced Composites (CFRCs) After Impact
inferred← citeshttps://doi.org/10.1007/s10443-021-09909-8openalex-snapshot
Analytical Solutions to Predict Impact Behaviour of Stringer Stiffened Composite Aircraft Panels
inferred← citeshttps://doi.org/10.1007/s10443-024-10272-7openalex-snapshot
Effect of Embedded Shape Memory Alloy (SMA) on the Low-velocity Impact Behaviour of Stringer Stiffened Composite Plates
inferred← citeshttps://doi.org/10.1007/s12046-020-01550-8openalex-snapshot
Effects of stiffener geometric parameters on the buckling and post-buckling response of composite I-stiffened panels
inferred← citeshttps://doi.org/10.1007/s40870-019-00194-yopenalex-snapshot
Low Velocity Response of GFRP and Hybrid Laminates Under Impact Testing
inferred← citeshttps://doi.org/10.1007/s42417-026-02799-9openalex-snapshot
Post-Impact Vibration Response of T-Stiffened Curved CFRP Panels: Parametric Finite Element Analysis and ANN-Assisted Prediction
inferred← citeshttps://doi.org/10.1007/s43995-025-00197-yopenalex-snapshot
Failure assessment of the engineered composite stiffened plates with geometric variations under high velocity impact by nonlinear finite element approach
inferred← citeshttps://doi.org/10.1016/j.ast.2024.109454openalex-snapshot
A novel integrated modeling strategy for predicting damage mechanisms and energy dissipation of composite stiffened structures under low-velocity impact and compression
inferred← citeshttps://doi.org/10.1016/j.compositesb.2018.05.034openalex-snapshot
Dynamic behavior of top-hat bonded stiffened composite panels: Experimental characterization
inferred← citeshttps://doi.org/10.1016/j.compositesb.2019.01.006openalex-snapshot
Damage and failure mechanism of thin composite laminates under low-velocity impact and compression-after-impact loading conditions
inferred← citeshttps://doi.org/10.1016/j.compstruct.2017.11.079openalex-snapshot
Modelling and simulating of the compressive behavior of T-stiffened composite panels subjected to stiffener impact
inferred← citeshttps://doi.org/10.1016/j.compstruct.2018.04.041openalex-snapshot
GF/epoxy laminates embedded with wire nets: A way to improve the low-velocity impact resistance and energy absorption ability
inferred← citeshttps://doi.org/10.1016/j.compstruct.2018.07.038openalex-snapshot
Experiment investigation on impact damage and influences on compression behaviors of single T-stiffened composite panels
inferred← citeshttps://doi.org/10.1016/j.compstruct.2018.08.080openalex-snapshot
Experimental study on delamination growth of stiffened composite panels in compression after impact
inferred← citeshttps://doi.org/10.1016/j.compstruct.2018.09.102openalex-snapshot
Filler materials in composite out-of-plane joints – A review
inferred← citeshttps://doi.org/10.1016/j.compstruct.2021.114640openalex-snapshot
Investigation on impact damage and shear after impact (SAI) behavior of grid stiffened panels
inferred← citeshttps://doi.org/10.1016/j.compstruct.2023.117722openalex-snapshot
Mechanical properties and failure behaviors of T1100/5405 composite T-joint under in-plane shear load coupled with initial defect and high-temperature
inferred← citeshttps://doi.org/10.1016/j.oceaneng.2020.106991openalex-snapshot
Experimental and numerical study on compression-after-impact behavior of composite panels with foam-filled hat-stiffener
inferred← citeshttps://doi.org/10.1016/j.tws.2022.109288openalex-snapshot
Study of impact damage on composite laminates induced by strip impactor using DIC and infrared thermography
inferred← citeshttps://doi.org/10.1016/j.tws.2022.109454openalex-snapshot
Experimental behavior and shear bearing capacity simulation of stiffened composite panels subjected to invisible damage impact
inferred← citeshttps://doi.org/10.1016/j.tws.2022.109705openalex-snapshot
Effects of fillers on the impact damage and compressive residual properties of single hat-stiffened composite panels
inferred← citeshttps://doi.org/10.1016/j.tws.2024.112525openalex-snapshot
Buckling and post-buckling analysis of composite stiffened panels: A ten-year review (2014–2023)
inferred← citeshttps://doi.org/10.1016/j.tws.2025.114276openalex-snapshot
An experimental and numerical study on the multi-point low-velocity impact and CAI of composite T-stiffened panels
inferred← citeshttps://doi.org/10.1016/j.tws.2025.114413openalex-snapshot
Quasi-static compressive behavior of CFRP composite plates with boundary unconstrained T-shaped stiffening ribs
inferred← citeshttps://doi.org/10.1080/01694243.2020.1844435openalex-snapshot
Influence of adhesive interface properties on the post-buckling response of composite I-stiffened panels with lateral support under axial compression
inferred← citeshttps://doi.org/10.1080/14484846.2019.1600212openalex-snapshot
Prediction of impact response of delaminated pretwisted stiffened shell
inferred← citeshttps://doi.org/10.1080/15397734.2025.2469134openalex-snapshot
Stiffened composite plates as equivalent structures for sandwich panels under low-velocity hail impact
inferred← citeshttps://doi.org/10.1108/aeat-03-2025-0110openalex-snapshot
Design optimization of aerospace-grade stiffened composite panels for low-velocity impact using the Taguchi L9 method
inferred← citeshttps://doi.org/10.1108/mmms-11-2022-0255openalex-snapshot
The research of buckling and post-buckling behavior of bidirectional stiffened composite panel under discrete impact
inferred← citeshttps://doi.org/10.1177/0040517519871259openalex-snapshot
A review on the mechanical properties of textile structural composite T-beams
inferred← citeshttps://doi.org/10.14419/ijet.v7i4.26.22162openalex-snapshot
Modeling Analysis of Guided Ultrasonic Waves in Composite Plates with Impact Damage
inferred← citeshttps://doi.org/10.1680/jemmr.24.00211openalex-snapshot
Numerical study on the failure mechanism of GFRP T-joint under low-velocity impact
inferred← citeshttps://doi.org/10.3390/aerospace10040327openalex-snapshot
Design and Testing of Impacted Stiffened CFRP Panels under Compression with the VERTEX Test Rig
inferred← citeshttps://doi.org/10.3390/polym18101259openalex-snapshot
Surface Glass Fiber Hybridization for Enhanced Low-Velocity Impact Resistance in CFRP T-Stiffened Panels
inferred← citeshttps://doi.org/10.3390/sym17040570openalex-snapshot
Impact and Post-Impact Compression Buckling Behavior of Symmetrical Foam-Filled Hat-Stiffened Panels
inferred← citeshttps://doi.org/10.55546/jmm.1459415openalex-snapshot
Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle
Editorial review for independent work. ICSAC — the Institute for Complexity
Science and Advanced Computing — runs a structured editorial panel for researchers
publishing outside journals, and publishes on CiteStamp rails. Submission is free
and goes through ORCID: icsacinstitute.org/submit.