Skin friction and heat transfer in hypersonic transitional and turbulent
boundary layers
Skin friction and heat transfer in hypersonic transitional and turbulent
boundary layers
The decompositions of the skin-friction and heat transfer coefficients based on the two-fold repeated integration in hypersonic transitional and turbulent boundary layers are analyzed to explain the generations of the wall skin friction and heat transfer. The Reynolds analogy factor slightly increases as the wall temperature decreases, especially for the …