Dynamics of Hydrofoils as Applied to Naval Propellers 



Table 1 

 Half Ordinates-NASA 16-66-66 Mod 



If direction is disregarded, the velocity increments are the same both on 

 the face and on the back, at each particular station along the chord. By applying 

 Bernoulli's equation between any couple of symmetrical points m and m' on the 

 foil surface, at which the pressure is assumed to be Pf, and p^, the following 

 relation is obtained: 



Pf - Pb 



1_ , - 4(l + A'K,)^A'V, ^+ A'V^C^^ 



pV 



(1) 



1021 



