A Highly Accurate Approach for Aeroelastic System with Hysteresis Nonlinearity

<div>Time histories of the aeroelastic system at <i>U</i>/<i>U</i><sub>0</sub> = 0.1 obtained by the exact solutions, PIM with the time step as 0.1, and RK with the time step as 0.1, 0.01, or 0.001, respectively.</div>

International Journal of Aerospace Engineering

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Figure 11

Figure 11: A Highly Accurate Approach for Aeroelastic System with Hysteresis Nonlinearity 