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Residual Strength and Fatigue Lifetime of ... - Solid Mechanics

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4.2 The Cycle Jump Method<br />

In structures subjected to cyclic loading, parameters, such as deflection, stress, strain, material<br />

properties <strong>and</strong>/or geometry (for example cracks), typically evolve over time. This evolution<br />

results in both global <strong>and</strong> local changes <strong>of</strong> the structural behaviour, where the global changes<br />

correspond to a general long-term trend, which can be expressed in terms <strong>of</strong> mathematical<br />

functions. Based on these mathematical functions, extrapolation schemes can be employed to<br />

determine the long-term response <strong>of</strong> the structure. Such an extrapolation scheme can be used in<br />

numerical simulations to accelerate the analysis <strong>and</strong> make it computationally effective. The cycle<br />

jump scheme developed by Cojocaru et al. (2006) will be summarised here for the completeness<br />

<strong>of</strong> the presentation. As proposed by Cojocaru et al. in order to accelerate fatigue simulation, a set<br />

<strong>of</strong> initial load cycles is simulated, using the finite element method, <strong>and</strong> the global evolution<br />

function is established for each state variable monitored. This global evolution function is then<br />

used to extrapolate the state variables over a number <strong>of</strong> cycles. The key question here is the<br />

accuracy <strong>of</strong> the extrapolated variables. To examine <strong>and</strong> control the accuracy <strong>of</strong> the extrapolations<br />

the number <strong>of</strong> jump cycles is determined by a criterion with a control parameter. The determined<br />

extrapolated state is used as an initial state for additional finite element simulations <strong>and</strong> next<br />

cycle jumps, see Figure 4.1.<br />

Figure 4.1: Schematic presentation <strong>of</strong> the cycle jump method, after Cojocaru et al. (2006).<br />

Assuming that a finite element analysis has been conducted for at least three computed load<br />

cycles, see Figure 4.2, for each state variable monitored, y=y(t), where t is time, the discrete<br />

slope can be defined for every two adjacent cycles as<br />

65

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