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Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels

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What this work says

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

inferredcites →https://doi.org/10.1016/0045-7949(80)90142-xopenalex-snapshot
Dynamic large deflection analysis of plates using mixed finite elements
inferredcites →https://doi.org/10.1016/0045-7949(80)90178-9openalex-snapshot
Postbuckling behaviour of plates and shells using a mindlin shallow shell formulation
inferredcites →https://doi.org/10.1016/0045-7949(91)90025-hopenalex-snapshot
Finite element analysis of supersonic flutter of multibay composite panels
inferredcites →https://doi.org/10.1016/j.compstruct.2007.01.007openalex-snapshot
Supersonic flutter characteristics of composite cylindrical panels
inferredcites →https://doi.org/10.1016/j.compstruct.2015.12.056openalex-snapshot
Flutter of stiffened composite panels considering the stiffener’s base as a structural element
inferredcites →https://doi.org/10.1016/j.compstruct.2017.07.042openalex-snapshot
Nonlinear aeroelastic analysis of curved laminated composite panels
inferredcites →https://doi.org/10.1016/j.compstruct.2017.08.058openalex-snapshot
Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime
inferredcites →https://doi.org/10.1016/j.ijnonlinmec.2021.103730openalex-snapshot
Nonlinear supersonic flutter of multibay cross-stream shallow shells
inferredcites →https://doi.org/10.1016/j.jfluidstructs.2011.12.011openalex-snapshot
Panel flutter at low supersonic speeds
inferredcites →https://doi.org/10.1016/j.jfluidstructs.2015.05.005openalex-snapshot
Nonlinear single-mode and multi-mode panel flutter oscillations at low supersonic speeds
inferredcites →https://doi.org/10.1016/j.jmatprotec.2004.02.063openalex-snapshot
Material cyclic behaviour of panels at supersonic speeds
inferredcites →https://doi.org/10.1016/j.jsv.2009.03.027openalex-snapshot
Aero-thermo-mechanical characteristics of imperfect shape memory alloy hybrid composite panels
inferredcites →https://doi.org/10.1016/j.jsv.2018.07.042openalex-snapshot
Finite element analysis of fluttering plates reinforced by flexible beams: An energy-based approach
inferredcites →https://doi.org/10.1016/j.tws.2020.107379openalex-snapshot
The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays
inferredcites →https://doi.org/10.1061/(asce)0733-9399(1984)110:5(794)openalex-snapshot
Exact Solutions of Moderately Thick Laminated Shells
inferredcites →https://doi.org/10.1115/1.3098919openalex-snapshot
Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds
inferredcites →https://doi.org/10.1177/002199837200600301openalex-snapshot
Stress Analysis of Thick Laminated Composite and Sandwich Plates
inferredcites →https://doi.org/10.2514/1.j054013openalex-snapshot
Development and Validation of a Fluid–Structure Solver for Transonic Panel Flutter
inferredcites →https://doi.org/10.2514/1.j057909openalex-snapshot
Correlation of Experimental and Computational Results for Flutter of Streamwise Curved Plate
inferredcites →https://doi.org/10.2514/3.11606openalex-snapshot
Finite element analysis of large-amplitude panel flutter of thin laminates
inferredcites →https://doi.org/10.2514/3.55195openalex-snapshot
Stability of Finite-Difference Equation for the Transient Response of a Flat Plate
inferredcites →https://doi.org/10.2514/3.5653openalex-snapshot
Nonlinear flutter of curved plates. II
inferredcites →https://doi.org/10.2514/3.6832openalex-snapshot
Natural vibration and flutter of cylindrically curved panels.
inferredcites →https://doi.org/10.2514/6.1993-1318openalex-snapshot
Hypersonic flutter of a curved shallow panel with aerodynamic heating
inferredcites →https://doi.org/10.2514/8.9264openalex-snapshot
The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical Shells

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.4907190openalex-extracted
Investigation of Limit Cycle Oscillations and Phase Portraits in Gfrp Based Composite Structures Embedded with Superelastic Shape Memory Alloy Wires
inferred← citeshttps://doi.org/10.1016/j.ast.2026.112902openalex-snapshot
Nonlinear aero-thermo-elastic analysis of multi-bay composite curved panels in cross-stream supersonic flow
inferred← citeshttps://doi.org/10.1016/j.cja.2025.103669openalex-snapshot
Accurate closed-form flutter eigensolutions of three-dimensional composite laminates with shear deformation
inferred← citeshttps://doi.org/10.1016/j.cma.2026.119343openalex-snapshot
Model reduction for nonlinear flutter analysis of panels in supersonic airflow based on mixed-mode spectral submanifolds
inferred← citeshttps://doi.org/10.1016/j.compstruct.2023.117138openalex-snapshot
Nonlinear static/dynamic behaviors of composite curved panels with piezoelectric patches in supersonic airflow
inferred← citeshttps://doi.org/10.1016/j.jcomc.2023.100361openalex-snapshot
Vibration and flutter analysis of damaged composite plates under thermal environment and its passive control using piezoelectric patches
inferred← citeshttps://doi.org/10.1016/j.tws.2025.113547openalex-snapshot
Nonlinear aeroelastic analysis of a skew reinforced composite panel
inferred← citeshttps://doi.org/10.1080/15376494.2022.2134611openalex-snapshot
Active flutter suppression of damaged variable stiffness laminated composite rectangular plate with piezoelectric patches
inferred← citeshttps://doi.org/10.1088/1361-665x/ae65eeopenalex-snapshot
A multi-method investigation of high-aspect-ratio natural fiber-SMA composite wings: flutter delay, vibration suppression, and nonlinear surrogate modeling
inferred← citeshttps://doi.org/10.1142/s0219455425500890openalex-snapshot
Exact Eigensolutions of Two-Dimensional Laminated Panel Flutter Based on Mindlin Plate Theory and the First-Order Piston Theory
inferred← citeshttps://doi.org/10.2339/politeknik.1622599openalex-snapshot
A Dynamic Instability Study of Shallow Shell Panels with Simply Supported Edges
inferred← citeshttps://doi.org/10.2514/1.c038325openalex-snapshot
Nonlinear Dynamics of Nitinol-Enhanced Carbon-Fiber-Reinforced Polymer Beam-Rod in Subsonic Flow
inferred← citeshttps://doi.org/10.2514/1.j064177openalex-snapshot
Bifurcation Analysis of Single-Bay Supersonic Panels Using Preflutter Output Data
inferred← citeshttps://doi.org/10.2514/6.2024-0190openalex-snapshot
Limit-Cycle Oscillation Prediction in Supersonic Panels Using Pre-Flutter Transient Responses
inferred← citeshttps://doi.org/10.2514/6.2025-1013openalex-snapshot
Fluid-Structure Interaction Analysis of a Compliant CFCF Panel at Mach 5.85
inferred← citeshttps://doi.org/10.2514/6.2026-0190openalex-snapshot
Numerical Investigation of the Aeroelastic Response of a CFCF Compliant Panel in Hypersonic Flow
inferred← citeshttps://doi.org/10.3390/sym14061154openalex-snapshot
Aeroelastic Topology Optimization of Wing Structure Based on Moving Boundary Meshfree Method
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