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On the Impact of Surface Thermal Conditions on Aero-heating to Hypersonic Vehicle

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Numerical simulation predicts heat flux in hypersonic vehicles, suggesting thermal conditions critically affect design.

Heat flux distribution is influenced by variations in wall temperature and nose radius, critical for vehicle design.
The model validated computational results against experimental data, ensuring prediction reliability.
Incorporating thermal non-equilibrium real gas properties enhances accuracy in predicting heat transfer dynamics.
Dynamic viscosity and thermal conductivity were established through non-equilibrium kinetic theory for accurate gas modeling.

Yassin et al. (2025) studied this question.

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