Proceedings of CETA 2026: Numerical Investigation
The research paper detailing the investigation of aerodynamic characteristics and shock wave behavior correlated with pressure distributions 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 [p.59].
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.