F,5 • NUMERICAL RESULTS 



0.86 



0.85 



0.84 



0.83 



0.82 



0.81 



4 6 8 10 12 14 16 



Mach number Me 



Fig. F,5k. Recovery factor for a laminar boundary layer on a flat plate in free flight 

 for various wall-to-free stream enthalpy ratios. Te = 400°R. 



0.86 



0.85 



0.84 



0.83 



0.82 



0.81 



12 3 4 5 6 



Enthalpy ratio h* (0) 



Fig. F,51. Recovery factor for a laminar boundary layer on a flat 

 plate in free flight for various Mach numbers. Tq = 400°R. 



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