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> = 0.85 in pitch direction provided by PIM, RK, and exact solutions, respectively.</div>

International Journal of Aerospace Engineering

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Figure 10

Figure 10: A Highly Accurate Approach for Aeroelastic System with Hysteresis Nonlinearity 