Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel. Advances in Applied Mathematics and Mechanics, [S. l.], v. 10, n. 5, p. 1158–1172, 2018. DOI: 10.4208/aamm.OA-2017-0342. Disponível em: https://www.global-sci.com/aamm/article/view/4981. Acesso em: 18 apr. 2026.