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Shell Model Reconstruction of Thin-Walled Structures from Point Clouds for Finite Element Modelling of Existing Steel Bridges. [PDF]
Sensors (Basel)Nakamizo T, Nishio M.
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ANALYSIS OF THIN WALLED CURVED BEAM
Transactions of the Japan Society of Civil Engineers, 1964 openaire +2 more sources
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Thin-walled beams in frame synthesis.
AIAA Journal, 1972References 1 Yang, H. T., "Lift of Wing-Body Combination," AIAA Journal, Vol. 10, No. 11, Nov. 1972, pp. 1535-1536. 2 Miles, J. W., "On Interference Factors for Finned Bodies," Journal of the Aeronautical Sciences, Vol. 18, No. 4, April 1952, p. 287. 3 Spreiter, J.
RICHARD B. NELSON, LEWIS P. FELTON
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Statics of thin‐walled pretwisted beams
International Journal for Numerical Methods in Engineering, 1981AbstractThe displacement and strain fields of thin‐walled pretwisted beams are prescribed in terms of generalized displacements for extension, bending, torsion and warping. Differential equations and boundary conditions are obtained from the elastic potential energy functional without assuming coincidence of the beam axis with any of the structural ...
Krenk, S., Gunneskov, O.
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Thin Walled Beams with Residual Stress
Journal of Elasticity, 2009zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Della Longa, Luca, Londero, Alessandro
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Anisotropic Inhomogeneous Rectangular Thin-Walled Beams
SIAM Journal on Mathematical Analysis, 2009This paper is devoted to the asymptotic analysis of the problem of linear elasticity for an anisotropic and inhomogeneous body occupying, in its reference configuration, a cylindrical domain with a rectangular cross section with sides proportional to $\varepsilon$ and $\varepsilon^2$ and clamped on one of its bases.
Lorenzo Freddi +2 more
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Distortion of thin-walled beams
Thin-Walled Structures, 2004First order Generalized Beam Theory (GBT) describes the behaviour of prismatic thin-walled structural members by using system of ordinary differential equations. Solution can lead to separation of the load components and then to subsequent combination of the stresses and deformations.
Stanislav Rendek, Ivan Baláž
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2009
Typical aeronautical structures involve light-weight, thin-walled, beam-like structures that must operate in a complex loading environment where combined axial, bending, shearing, and torsional loads are present. These structures may consist of closed or open sections, or a combination of both.
Bauchau, Olivier, Craig, JI
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Typical aeronautical structures involve light-weight, thin-walled, beam-like structures that must operate in a complex loading environment where combined axial, bending, shearing, and torsional loads are present. These structures may consist of closed or open sections, or a combination of both.
Bauchau, Olivier, Craig, JI
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A beam theory for thin-walled composite beams
Composites Science and Technology, 1988Abstract A beam theory is presented that is formulated in terms of the in-plane elastic properties of the panels of the cross-section of a thin-walled composite beam. Shear deformation is accounted for by using a suitable form of the Timoshenko beam theory together with a modified form of the shear coefficient.
L.C. Bank, P.J. Bednarczyk
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A NONLINEAR THEORY OF GENERAL THIN-WALLED BEAMS
Computers & Structures, 1981Abstract A complete and consistent theory is formulated to describe the large-deflection elastic-plastic behavior of thin-walled beams of arbitrary initial shape and subjected to arbitrary transient loadings. The nonlinear beam theory is derived from a well-documented nonlinear shell theory through an application of Hamilton's Principle.
Meredith, D., Witmer, E. A.
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