Proceedings of CETA 2026: Numerical Investigation
The research paper detailing the investigation of aerodynamic characteristics and shock wave behavior of the swept-wing has been officially published within the proceedings of the CETA 2026 conference. This numerical investigation addresses the geometric parameterizations of specialized airfoils, specifically evaluating the SC(2)-0410 geometries.
Analytical approaches were rigorously utilized to validate the numerical solutions extracted from Finite Volume Methods (FVM), executing discrete governing equations across computational platforms such as Ansys Fluent and SU2.