F • CONVECTIVE HEAT TRANSFER IN GASES 



Sins 



0.82 



0.81 



0.80 



0.79 



0.78 



0.77 



2 4 6 8 10 12 14 16 



Mach number Me 



Fig. F,5m. Reynolds analogy factor for a laminar boundary layer 

 on an insulated flat plate in free flight. Te = 400°R. 



0.82 



0.81 



0.80 



0.79 



0.78 



0.77 



4.6 8 10 12 14 16 



Mach number Ma 



Fig. F,5n. Reynolds analogy factor for a laminar boundary layer on a flat plate in 

 free flight for various wall-to-free stream enthalpy ratios. T^ = 400°R. 



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