A Highly Accurate Approach for Aeroelastic System with Hysteresis Nonlinearity

<div>Logarithmic errors of modified Euler, Newmark, or PIM results with respect to the exact solutions of the aeroelastic system at <i>U</i>/<i>U</i><sub>0</sub> = 0.9 in pitch direction.</div>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: A Highly Accurate Approach for Aeroelastic System with Hysteresis Nonlinearity 