A Mach 6 blunt-cone heating simulation with generic CFD and heat-conduction solvers is presented, but the paper provides no quantitative validation and contains internal inconsistencies.
Hypersonic Laminar -Turbulent Transition on Circular Cones and Scramjet Forebodies
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Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone
A Mach 6 blunt-cone heating simulation with generic CFD and heat-conduction solvers is presented, but the paper provides no quantitative validation and contains internal inconsistencies.