AIAA Journal · 1980 · 413 citations · 14 references
EngineeringCivil EngineeringComputational EngineeringComputational MechanicsFinite Element AnalysisFinite Element MethodsFinite Element FormulationNonlinear Finite Element AnalysisNonlinear Structural AnalysisStructural Finite Element AnalysisStructural Response AnalysisStructural SimulationDisplacementFinite Element ModelingLagrangian FormulationNonlinear AnalysisNonlinear Static AnalysisPerturbation ModelingStatic Structural ResponseStep Size Selection
The authors present a reduced basis technique and computational algorithm for predicting the nonlinear static response of structures. The method uses a total Lagrangian finite‑element discretization, represents nodal displacements as a linear combination of a few basis vectors, and applies Rayleigh–Ritz to reduce the equations to a small nonlinear system, with basis functions chosen from the static perturbation technique and an automatic load‑step selection that monitors accuracy. Numerical examples confirm the high accuracy and effectiveness of the proposed reduced‑basis approach.
A reduced basis technique and a computational' algorithm are presented for predicting the nonlinear static response of structures. A total Lagrangian formulation is used and the structure is discretized by using displacement finite element models. The nodal displacement vector is expressed as a linear combination of a small number of basis vectors and a Rayleigh-Ritz technique is used to approximate the finite element equations by a reduced system of nonlinear equations. The Rayleigh-Ritz approximation functions (basis vectors) are chosen to be those commonly used in the static perturbation technique namely, a nonlinear solution and a number of its path derivatives. A procedure is outlined for automatically selecting the load (or displacement) step size and monitoring the solution accuracy. The high accuracy and effectiveness of the proposed approach is demonstrated by means of numerical examples.
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An approximate analysis technique for design calculations
R. L. Fox, H. MlURA · AIAA Journal · 1971 · 105 citations