F • CONVECTIVE HEAT TRANSFER IN GASES 

 0.88 



0.87 



0.86 



0.85 



0.84 



0.83 



1 2 3 4 5 6 



Mach number Me 



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

 flat plate in a wind tunnel at a supply temperature of 100°F. 



0.84 



0.83 



0.82 



0.81 



0.80 



0.79 



1 2 3 4 5 6 



Mach number Me 



Fig. F,5r. Reynolds analogy factor for a laminar boundary layer^on an 

 insulated flat plate in a wind tunnel at a supply temperature of 100°F. 



( 360 > 



