On the public citation graph

Dynamics of Composite Aircraft Wings Carrying External Stores

https://doi.org/10.2514/1.25541
0 signed · 47 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.
Claim with ORCID
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 See whether every reference in this work resolves to a known work and none has been retracted — and get a dated CiteStamped badge you can embed.
See reference health

What this work says

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

inferredcites →https://doi.org/10.1006/jsvi.1993.1325openalex-snapshot
Free Vibration Of Anisotropic Composite Thin-Walled Beams Of Closed Cross-Section Contour
inferredcites →https://doi.org/10.1006/jsvi.1999.2627openalex-snapshot
DYNAMIC RESPONSE OF ADAPTIVE CANTILEVERS CARRYING EXTERNAL STORES AND SUBJECTED TO BLAST LOADING
inferredcites →https://doi.org/10.1007/1-4020-4203-5openalex-snapshot
Thin-Walled Composite Beams: Theory and Application
inferredcites →https://doi.org/10.1007/s00707-009-0248-2openalex-snapshot
Divergence and flutter of shear deformable aircraft swept wings subjected to roll angular velocity
inferredcites →https://doi.org/10.1016/0020-7403(95)00075-5openalex-snapshot
Bending vibrations of adaptive cantilevers with external stores
inferredcites →https://doi.org/10.1016/0045-7949(93)90246-aopenalex-snapshot
Vibration analysis of composite wing with tip mass using finite elements
inferredcites →https://doi.org/10.1016/j.jsv.2009.01.002openalex-snapshot
Bending-torsional flutter of wings with an attached mass subjected to a follower force
inferredcites →https://doi.org/10.1016/s0263-8223(02)00019-3openalex-snapshot
On a shear-deformable theory of anisotropic thin-walled beams: further contribution and validations
inferredcites →https://doi.org/10.1016/s0734-743x(98)00019-0openalex-snapshot
DYNAMIC RESPONSE OF ANISOTROPIC THIN-WALLED BEAMS TO BLAST AND HARMONICALLY OSCILLATING LOADS
inferredcites →https://doi.org/10.1016/s1270-9638(98)80008-4openalex-snapshot
Effects of externally mounted stores on aeroelasticity of advanced swept cantilevered aircraft wings
inferredcites →https://doi.org/10.1017/s0001924000003328openalex-snapshot
The effect of multiple stores arrangement on flutter speed of a shear deformable wing subjected to pull-up angular velocity
inferredcites →https://doi.org/10.1061/(asce)as.1943-5525.0000037openalex-snapshot
Flutter of a Swept Aircraft Wing with a Powered Engine
inferredcites →https://doi.org/10.1106/ld1r-whmw-jp4k-nqqxopenalex-snapshot
Optimal Dynamic Response Control of Adaptive Thin-Walled Cantilevers Carrying Heavy Stores and Exposed to Blast Pulses
inferredcites →https://doi.org/10.1115/1.3423921openalex-snapshot
Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures
inferredcites →https://doi.org/10.1121/1.420397openalex-snapshot
Vibration and dynamic response control of cantilevers carrying externally mounted stores
inferredcites →https://doi.org/10.1142/3092-part1openalex-snapshot
Structronic Systems: Smart Structures, Devices and Systems
inferredcites →https://doi.org/10.1177/1045389x9400500105openalex-snapshot
Adaptive Response Control of Cantilevered Thin-Walled Beams Carrying Heavy Concentrated Masses
inferredcites →https://doi.org/10.2514/1.40463openalex-snapshot
Effects of Rolling Maneuver on Divergence and Flutter of Aircraft Wing Store
inferredcites →https://doi.org/10.2514/2.2718openalex-snapshot
Aeroelastic Tailoring of Composite Wings Exhibiting Nonclassical Effects and Carrying External Stores
inferredcites →https://doi.org/10.2514/2.499openalex-snapshot
Static and Dynamic Aeroelasticity of Advanced Aircraft Wings Carrying External Stores
inferredcites →https://doi.org/10.2514/3.13141openalex-snapshot
Nonclassical effects on divergence and flutter of anisotropic swept aircraft wings
inferredcites →https://doi.org/10.2514/3.46551openalex-snapshot
Comprehensive model of anisotropic composite aircraft wings suitable for aeroelastic analyses
inferredcites →https://doi.org/10.4050/jahs.35.42openalex-snapshot
Nonclassical Behavior of Thin‐Walled Composite Beams with Closed Cross Sections

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.4803636openalex-extracted
Vibration Analysis and Active Control of Irregular Integrated Composite Sandwich Plates with Incompletely Constrained Boundaries
inferred← citeshttps://doi.org/10.1007/s00158-026-04311-zopenalex-snapshot
Parallelized complex method for multidisciplinary optimization of aeroelastic performance in thin-walled wing–engine system using bidirectional curvilinear fiber pathing
inferred← citeshttps://doi.org/10.1007/s00707-009-0248-2openalex-snapshot
Divergence and flutter of shear deformable aircraft swept wings subjected to roll angular velocity
inferred← citeshttps://doi.org/10.1007/s40430-015-0436-zopenalex-snapshot
Experimental investigation of linear and nonlinear aeroelastic behavior of a cropped delta wing with store in low subsonic flow
inferred← citeshttps://doi.org/10.1007/s42405-018-0034-2openalex-snapshot
Frequency Analysis of Wing–Rotor System Considering Flexibility in Capsule Based on High-Accurate Method
inferred← citeshttps://doi.org/10.1016/j.apm.2026.116783openalex-snapshot
Analytical dynamic modeling and aeroelastic stability of arbitrarily restrained aerospace composite structure with stiffener and external store
inferred← citeshttps://doi.org/10.1016/j.ast.2019.105353openalex-snapshot
Flutter improvement of a thin walled wing-engine system by applying curvilinear fiber path
inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2019.01.014openalex-snapshot
Structural and aeroelastic analyses of a wing with tip rotor
inferred← citeshttps://doi.org/10.1016/j.jsv.2009.01.002openalex-snapshot
Bending-torsional flutter of wings with an attached mass subjected to a follower force
inferred← citeshttps://doi.org/10.1016/j.tws.2025.113918openalex-snapshot
Analysis of modal and damping characteristics of irregular smart composite laminated plates under incompletely constrained boundaries
inferred← citeshttps://doi.org/10.1017/s0001924000003328openalex-snapshot
The effect of multiple stores arrangement on flutter speed of a shear deformable wing subjected to pull-up angular velocity
inferred← citeshttps://doi.org/10.1017/s0001924000009763openalex-snapshot
Vibration analyses of an equivalent plate wing with an external store
inferred← citeshttps://doi.org/10.1038/s41598-022-11211-xopenalex-snapshot
Torsional vibration analysis of shaft with multi inertias
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0000037openalex-snapshot
Flutter of a Swept Aircraft Wing with a Powered Engine
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0000157openalex-snapshot
Aeroelastic Modeling and Flutter Prediction of Swept Wings Carrying Twin Powered Engines
inferred← citeshttps://doi.org/10.1177/0954410015613615openalex-snapshot
Investigation of adding fins to external stores for improving the flutter characteristics of a wing/store configuration
inferred← citeshttps://doi.org/10.18178/ijmerr.8.3.477-482openalex-snapshot
Coupled Bending-Torsional Dynamic Behavior of a Cantilever Beam Carrying Multiple Point Masses
inferred← citeshttps://doi.org/10.20855/ijav.2016.21.3427openalex-snapshot
Aeroelastic Analysis of Unrestrained Aircraft Wing with External Stores Under Roll Maneuver
inferred← citeshttps://doi.org/10.2514/1.40463openalex-snapshot
Effects of Rolling Maneuver on Divergence and Flutter of Aircraft Wing Store
inferred← citeshttps://doi.org/10.2514/1.c031080openalex-snapshot
Flutter of Aircraft Wings Carrying a Powered Engine Under Roll Maneuver
inferred← citeshttps://doi.org/10.2514/1.j057582openalex-snapshot
Nonlinear Modal Interactions of Swept Composite Aircraft Wings Carrying External Stores
inferred← citeshttps://doi.org/10.30518/jav.668240openalex-snapshot
Sequential Quadratic Optimization of Aeroelastic Energy of Twin-Engine Wing System with Curvilinear Fiber Path
inferred← citeshttps://doi.org/10.4028/www.scientific.net/amr.853.453openalex-snapshot
Effects of Parameters on Flutter of a Wing with an External Store
inferred← citeshttps://doi.org/10.4028/www.scientific.net/amr.912-914.907openalex-snapshot
Limit Cycle Flutter Analysis of a High-Aspect-Ratio Wing with an External Store
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.