F,5 • NUMERICAL RESULTS 



0.88 

 0.87 

 0.86 



0.85- 



u 

 o 



X 0.84 

 CD 



^ 0.83 

 u 



<D 



Q^ 0.82 



0.81 



0.80 



4 6 8 



Mach number Me 



10 



12 



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

 flat plate in a wind tunnel at various supply temperatures. 



0.88 



0.87 



- 0.86 



O 0.85 



u 



o 



"i 0.84 



(U 



O 0.83 

 u 



O) 



0.82 

 0.81 



0.80 



500 1000 1500 



Supply temperature^ °F 



2000 



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

 flat plate in a heated wind tunnel for various Mach numbers. 



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