Volume 28, Issue 3 No AccessReview of composite rotor blade modelingDewey H. HodgesDewey H. Hodges Georgia Institute of Technology, Atlanta, GeorgiaSearch for more papers by this authorPublished Online:17 May 2012https://doi.org/10.2514/3.10430SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byPassive Blade-Vortex Interaction Noise Reduction Using In-Blade Resonator CavitiesDaniel Weitsman and Eric Greenwood4 January 2024Comparative Study of Soft In-Plane and Stiff In-Plane Tiltrotor Blade Aerodynamics in Conversion Flight, Using CFD-CSD Coupling Approach15 January 2024 | Aerospace, Vol. 11, No. 1A Review of Modeling of Composite Structures17 January 2024 | Materials, Vol. 17, No. 2Analysis of Thin-Walled Beams via a One-Dimensional Unified Formulation Through a Navier-Type Solution25 September 2023 | International Journal of Applied Mechanics, Vol. 15, No. 09Modeling of geometrical stiffening in a rotating blade—A reviewJournal of Sound and Vibration, Vol. 548Analytical prediction of the cross-sectional shear flow in non-prismatic inhomogeneous beamlike solidsThin-Walled Structures, Vol. 183A Review of Modeling of Composite StructuresWenbin Yu19 January 2023Closed-Form Analysis of Thin-Walled Composite Beams Using Mixed Variational Approach4 October 2022 | Aerospace, Vol. 9, No. 10Stress recovery of laminated non-prismatic beams under layerwise traction and body forces18 July 2022 | International Journal of Mechanics and Materials in Design, Vol. 18, No. 3Analytical evaluation of stresses and strains in inhomogeneous non-prismatic beams undergoing large deflections25 June 2022 | Acta Mechanica, Vol. 233, No. 7Dynamic Analysis of a Rotating Double-Tapered FGM Beam with Various Shear Models Using a Constrained Variational Method15 December 2021 | International Journal of Structural Stability and Dynamics, Vol. 22, No. 07Aeroelastic Optimization of the High Aspect Ratio Wing with AileronComputers, Materials & Continua, Vol. 70, No. 3Main rotor blade modeling approaches comparison. 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Hodges 17 May 2012 | AIAA Journal, Vol. 29, No. 11Periodic Response of Thin-Walled Composite Helicopter Rotor BladesJournal of the American Helicopter Society, Vol. 36, No. 4Free‐Vibration Analysis of Composite BeamsJournal of the American Helicopter Society, Vol. 36, No. 3Coupled deflection and rotation of anisotropic open-section composite stiffenersLAWRENCE BANK and EMMANUEL COFIE17 August 2012Application of the variational-asymptotical method to static and dynamic behavior of elastic beamsALI ATILGAN, DEWEY HODGES, MARK FULTON and CARLOS CESNIK17 August 2012Tailoring of composite wing structures for elastically produced camber deformationsLAWRENCE REHFIELD, STEPHEN CHANG, PETER ZISCHKA, RICHARD PICKINGS and MICHAEL HOLL17 August 2012A survey and comparison of engineering beam theories for helicopter rotor bladesDONALD KUNZ17 August 2012Helicopter rotor blade aeroelasticity in forward flight with an implicit structural formulationROBERTO CELI17 August 2012Nonclassical Behavior of Thin‐Walled Composite Beams with Closed Cross SectionsJournal of the American Helicopter Society, Vol. 35, No. 2Rotating Thin-Walled Anisotropic Beams What's Popular Volume 28, Number 3March 1990 Metrics Crossmark TopicsComposite MaterialsComposite StructuresContinuum MechanicsDeformationFatigue (Materials)Material PropertiesMaterialsMaterials and Structural MechanicsMechanical PropertiesSolid MechanicsStructural Dynamics and CharacterizationStructural Material PropertiesStructural Mechanics KeywordsRotor BladesFinite Element AnalysisStress DistributionShear DeformationElastic PropertiesHelicopter BladeGraphical User InterfaceComposite MaterialsEuler Bernoulli BeamsCantilever BeamDigital Published online17 May 2012