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HI-Mach (Hypersonic Impact Method for Aerodynamics and Convective Heating) is a rapid, unstructured, hypersonic impact panel code currently being developed by the AeroLab at Utah State University. HI-Mach uses local inclination methods to predict the thermodynamic properties on the surfaces of arbitrary hypersonic bodies.

HI-Mach is currently under active development and is expected to be completed in 2025.