Assessment of beam modeling methods for rotor blade applications.
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Publication:5952778
DOI10.1016/S0895-7177(00)00302-2zbMath1197.74055WikidataQ126437987 ScholiaQ126437987MaRDI QIDQ5952778
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Publication date: 22 January 2002
Published in: Mathematical and Computer Modelling (Search for Journal in Brave)
Related Items (9)
Linear viscoelastic analysis of straight and curved thin-walled laminated composite beams ⋮ A Rankine-Timonshenko-Vlasov beam theory for anisotropic beams via an asymptotic strain energy transformation ⋮ Maximum stiffness and minimum weight optimization of laminated composite beams using continuous fiber angles ⋮ Free vibration and dynamic stability of rotating thin-walled composite beams ⋮ A three-unknown refined shear beam model for the bending of randomly oriented FG-CNT/fiber-reinforced composite laminated beams rested on a new variable elastic foundation ⋮ Equations of motion of rotating composite beam with a nonconstant rotation speed and an arbitrary preset angle ⋮ An asymptotic analysis of composite beams with kinematically corrected end effects ⋮ A moderate deflection composite helicopter rotor blade model with an improved cross-sectional analysis ⋮ Isogeometric analysis of composite beams with arbitrary cross-section using dimensional reduction method
Cites Work
- On the energy of an elastic rod
- Fundamental closed-form solutions for solid and thin-walled composite beams including a complete out-of-plane warping model
- Thick-walled composite beam theory including 3-D elastic effects and torsional warping
- Theory of Anisotropic Thin-Walled Beams
- Finite-Element Model for Composite Beams with Arbitrary Cross-Sectional Warping
- A new rectangular beam theory
- Anisotropic beam theory and applications
- Experimental and theoretical analysis of composite I-beams with elastic couplings
- Pure Bending, Stretching, and Twisting of Anisotropic Cylindrical Shells
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