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Global behaviour of a composite stiffened panel in buckling. Part 2: Experimental investigation

https://doi.org/10.1016/j.compstruct.2011.07.029

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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1016/0010-4361(95)91382-fopenalex-snapshot

Buckling and postbuckling of composite structures

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.compstruc.2007.04.022openalex-snapshot

Design and analysis of stiffened composite panels including post-buckling and collapse

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.2007.01.012openalex-snapshot

Degradation investigation in a postbuckling composite stiffened fuselage panel

inferredcites →https://doi.org/10.1016/j.compstruct.2009.04.001openalex-snapshot

Multi-level experimental and numerical analysis of composite stiffener debonding. Part 1: Non-specific specimen level

inferredcites →https://doi.org/10.1016/j.compstruct.2011.04.026openalex-snapshot

Global behaviour of a composite stiffened panel in buckling. Part 1: Numerical modelling

inferredcites →https://doi.org/10.1016/s1359-835x(99)00085-8openalex-snapshot

Postbuckling behaviour of a blade-stiffened composite panel loaded in uniaxial compression

inferredcites →https://doi.org/10.2514/1.18994openalex-snapshot

Design and Evaluation of Composite Fuselage Panels Subjected to Combined Loading Conditions

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

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Experimental Inwestigation of Compressed Beams / Columns Using Optical Methods

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In Lieu of Introduction

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Investigations on Buckling Behaviour of Laminated Curved Composite Stiffened Panels

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Experimental and FE analysis for the buckling behavior of hat-stiffened panels under edge compressive loading

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Effects of stiffener geometric parameters on the buckling and post-buckling response of composite I-stiffened panels

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Effect of Stringer Design on the Stability of Stiffened Composite Panel Under In-plane Shear: An Experimental Study

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Specific testing of textiles for transportation

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Damage investigation in CFRP composites using full-field measurement techniques: Combination of digital image stereo-correlation, infrared thermography and X-ray tomography

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Experiment and optimization of the hat-stringer-stiffened composite panels under axial compression

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Effect of the stiffener stiffness on the buckling and post-buckling behavior of stiffened composite panels – Experimental investigation

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Numerical and experimental value added of Multi-Instrumented Technological Evaluator for the analysis of thick monolithic composite structures with singularity details

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Buckling of 120° stiffened composite cylindrical shell under axial compression – Experiment and simulation

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Experimental and numerical analysis for the post-buckling behavior of stiffened composite panels with impact damage

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Influence of boundary conditions on the critical and failure load in the GFPR channel cross-section columns subjected to compression

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Remarks on experimental and theoretical investigations of buckling loads for laminated plated and shell structures

inferred← citeshttps://doi.org/10.1016/j.compstruct.2020.112132openalex-snapshot

Effects of hygrothermal environment on the buckling and postbuckling performances of stiffened composite panels under axial compression

inferred← citeshttps://doi.org/10.1016/j.compstruct.2021.114143openalex-snapshot

Review of digital image correlation application to large-scale composite structure testing

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.ijfatigue.2017.03.046openalex-snapshot

Investigation on impact damage evolution under fatigue load and shear-after-impact-fatigue (SAIF) behaviors of stiffened composite panels

inferred← citeshttps://doi.org/10.1016/j.paerosci.2015.05.008openalex-snapshot

Behavior of curved laminated composite panels and shells under axial compression

inferred← citeshttps://doi.org/10.1016/j.sna.2015.10.008openalex-snapshot

Monitoring of the curing process of composite structures by tunnelling junction sensors

inferred← citeshttps://doi.org/10.1016/j.tws.2014.08.008openalex-snapshot

Buckling measurement and numerical analysis of M-type ribs stiffened composite panel

inferred← citeshttps://doi.org/10.1016/j.tws.2015.12.026openalex-snapshot

Potential of cross section varying Ω stringer made of carbon fibre reinforced plastics

inferred← citeshttps://doi.org/10.1016/j.tws.2018.08.024openalex-snapshot

Buckling detection of an omega-stiffened aircraft composite panel using distributed fibre optic sensors

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Effect of discrete source damage on buckling and post-buckling behaviour of composite hat-stiffened panels under uniaxial compression

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/10.1080/15376494.2018.1495795openalex-snapshot

Buckling behavior of stiffened composite panels with variable thickness skin under compression

inferred← citeshttps://doi.org/10.1088/2631-8695/ad3893openalex-snapshot

A review on buckling of the laminated composite panel under in-plane load

inferred← citeshttps://doi.org/10.1177/14759217211001752openalex-snapshot

Damage assessment of a titanium skin adhesively bonded to carbon fiber–reinforced plastic omega stringers using acoustic emission

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Buckling Behavior of Poly-Phenylene-Sulfide/Carbon L-Shaped Stringers and a Stiffened Panel Obtained by Induction Welding

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Failure Analysis of Large-Scale Composite Fuselage Panels Under Combined Loads

inferred← citeshttps://doi.org/10.3390/ma14051271openalex-snapshot

Experimental Optical Testing and Numerical Verification by CuFSM of Compression Columns with Modified Channel Sections

inferred← citeshttps://doi.org/10.3390/polym15010165openalex-snapshot

An Experimental and Numerical Study on Impact and Compression after Impact of Stiffened Composite Panels

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Influence of Boundary Conditions on the Critical and Failure Load in the GFPR Channel Cross-Section Columns Subjected to Compression

inferred← citeshttps://doi.org/10.4172/2168-9792.1000209openalex-snapshot

Mechanical Behavior of a Fuselage Stiffened Carbon-Epoxy Panel under Debonding Load

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OPTICAL EXPERIMENTAL AND NUMERICAL STUDY ON THE COMPRESSION BUCKLING BEHAVIORS OF COMPOSITE PANEL STIFFENED BY I-TYPE RIBS

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