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1. Introduction Supersonic flows over aerodynamic shapes, such as wedges, play a pivotal role in modern aerospace engineering and aerodynamics. Understanding the complex flow patterns, shock wave interactions, and aerodynamic performance associated with these configurations is essential for the design and analysis of high-speed aircraft (e.g., electrical aircraft [1]) and space vehicles.
Improvements in turbine design methods have resulted in the development of blade profiles with both high lift and good Reynolds lapse characteristics. An increase in aerodynamic loading of blades in the low-pressure turbine (LPT) section of aircraft gas turbine engines has the potential to reduce engine weight or increase power extraction. Increased blade loading means larger pressure gradients and increased secondary losses near the endwall.
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