This document explores the aerothermal optimization of leading-edge geometries for hypersonic vehicles, which operate at speeds exceeding Mach 5 and encounter extreme aerodynamic and thermal challenges. The design of the leading edge is critical in managing the intense heat flux and aerodynamic forces that influence the vehicle's performance and structural integrity. Hypersonic vehicles face major challenges, including high levels of aerodynamic heating, material degradation under extreme conditions, and complex flow dynamics at these speeds.......
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