TABLE 3 (Continued) 

 TABLE 3C - THICKNESS AND CAMBER DISTRIBUTIONS USED FOR PROPELLERS 4679 AND 4718 



y 



yt* 



E It ** 



0.0000 



0.0000 



0.0000 



0.005 



0.0665 



0.0423 



0.0075 



0.0812 



0.0595 



0.0125 



0.1044 



0.0907 



0.025 



0.1466 



0.1586 



0.05 



0.2066 



0.2712 



0.075 



0.2525 



0.3657 



0.1 



0.2907 



0.4482 



0.15 



0.3521 



0.5869 



0.2 



0.4000 



0.6993 



0.25 



0.4363 



0.7905 



0.3 



0.4367 



0.8635 



0.35 



0.4832 



0.9202 



0.4 



0.4952 



0.9615 



0.45 



0.5 



0.9881 



0.5 



0.4962 



1.0 



0.55 



0.4846 



0.9971 



0.6 



0.4653 



0.9786 



0.65 



0.4383 



0.9434 



0.7 



0.4035 



0.8892 



0.75 



0.3612 



0.8121 



0.8 



0.3110 



0.7027 



0.85 



0.2532 



0.5425 



0.9 



0.1877 



0.3586 



0.95 



0.1143 



0.1713 



0.975 



0.0748 



0.0823 



1.0 



0.0333 







*NACA 66 Section (DTNSRDC modified). 



**NACA a = 0.8 meanline: the design procedure determines the magnitude 

 of the camber at each radius and uses the two-dimensional chordwise dis- 

 tribution of camber. 



205 



