Aeroelastic Analysis of Wings in the Transonic Regime: Planform’s Influence on the Dynamic Instability

<div>(a) The finite element model of the curved wing (upper and lower skins partially removed). (b) The finite element model of the curved wing (wing structure layout).</div>

International Journal of Aerospace Engineering

fig5

Figure 5

Figure 5: Aeroelastic Analysis of Wings in the Transonic Regime: Planform’s Influence on the Dynamic Instability 