The shock-boundary layer interaction is a complex phenomenon in fluid dynamics, particularly in high-speed aerodynamics. There isn’t a single formula to describe it, as it depends on various factors such as flow conditions, geometry, and boundary layer characteristics. However, researchers often use empirical correlations, numerical simulations, or theoretical models to study and predict these interactions.
Where:
- is the Nusselt number (heat transfer coefficient),
- ℎ is the convective heat transfer coefficient,
- is the characteristic length,
- is the thermal conductivity of the fluid