The drag of an airfoil at zero angle of attack is a function of density, viscosity, and velocity, in addition to a length parameter



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where
where
Solution Procedure:
(i) Determine

(ii) Assume a value for f using the Moody diagram. (Locate and move horizontally across the diagram to the f axis)



(iii) Using f calculate from

(iv) Use to determine Re from


(v) Using and Re, determine f
(vi) Compare f obtained in (v) with f assumed in (ii). If they are the same, STOP. If not, repeat steps (iii) through (vi) until convergence is attained

(vii) After convergence calculate the discharge using

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