1.
A DDG Method with a Residual-Based Artificial Viscosity for the Transonic/Supersonic Compressible Flow. Commun. Comput. Phys. [Internet]. 2022 Mar. 30 [cited 2026 Mar. 4];31(4):1134-61. Available from: https://www.global-sci.com/cicp/article/view/7058