F • CONVECTIVE HEAT TRANSFER IN GASES 

 0.86 



0.84 



S 0.82 



0.80 



0.78 



106 



10^ 



Re 



108 



Fig. F,lle. Reynolds analogy factor for a turbulent boundary layer 

 on a flat plate in air as a function of Reynolds number. Me = 0. 



0.83 



0.82 



0.81 



0.80 



0.79 



0.78 



Me 



Fig. Fjllf. Reynolds analogy factor for a turbulent boundary layer on a flat plate 

 in air in a wind tunnel as a function of Mach number. To = 100°F. 



< 380 > 



