F • CONVECTIVE HEAT TRANSFER IN GASES 



0.5 



0.4 



|<D 0.3 



00 0.2 



0.1 



2 4 6 8 10 12 14 16 



Mach number Me 



Fig. F,5i. Local heat transfer coefficient for a laminar boundary layer on a flat plate 

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



0.86 



0.85 



0.84 



0.83 



0.82 



0.81 



2 4 6 8 10 12 14 16 



Mach number Me 



Fig. F, 5j. Recovery factor for a laminar boundary layer on an 

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



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