International Journal of Aerospace Engineering / 2016 / Article / Fig 5

Research Article

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

Figure 5

(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).
(a)
(b)

Article of the Year Award: Outstanding research contributions of 2020, as selected by our Chief Editors. Read the winning articles.