Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel. Adv. Appl. Math. Mech. [Internet]. 2018 Sep. 17 [cited 2026 Apr. 18];10(5):1158-72. Available from: https://www.global-sci.com/aamm/article/view/4981