Continuous one-dimensional model of a spatial lattice. Deformation, vibration and buckling problems. (1st March 2019)

• Record Type: Journal Article
• Authors: Guzmán, A.M.; Rosales, M.B.; Filipich, C.P.
• Is Part Of: Engineering structures. Volume 182(2019)
• Page Start: 290
• Page End: 300
• Publication Date: 2019-03-01
• Subjects: Spatial lattice -- Continuous model -- Static -- Vibration -- Buckling; Structural engineering -- Periodicals; Structural analysis (Engineering) -- Periodicals; Construction, Technique de la -- Périodiques; Génie parasismique -- Périodiques; Pression du vent -- Périodiques; Earthquake engineering; Structural engineering; Wind-pressure; Periodicals; 624.105
• DOI: 10.1016/j.engstruct.2018.12.074
• Languages: English
• ISSNs: 0141-0296

Abstract

Highlights: The differential system is solved with low computational cost. The numerical results indicate a very good performance of the 6DE model proposed. The 6DE model allows to obtain the equivalent properties for the beam-column model. Practical expressions for the buckling loads exhibit an excellent agreement. Abstract: Lattice towers and guyed masts are frequently used in the telecommunication industry, particularly to support antennas. These structural systems comprise a large number of elements (mainly, legs and diagonals) and for this reason, their representation by equivalent models is quite common and convenient. In a previous study, the authors derived a continuous model of a spatial lattice governed by nine differential equations (9DE). The legs trace forms a triangle and the diagonals with a zig-zag pattern are contained in three planes that join each two legs, defined as Pattern 1. Here and starting from an energy statement, the structural behavior of a 1D continuous model governed by six differential equations (6DE) which leads to a simpler representation of the lattice structure, is stated. This formulation considers the shear flexibility and the second order effect due to axial loads. Also, the inertial forces due to the legs and diagonals masses are taken into account. Numerical examples dealing with deflections, critical buckling loads and natural frequencies are solved with this 1D model. The results are compared with the outcomes found with finite element methods. A very good performance is attained with the proposed model. Finally, the equivalent properties for other patterns of diagonalization (Patterns 2, 3 and 4) different to the studied as well as the formulas to find the critical loads are included in Appendices.