The aerodynamic characteristics of an S-cambered profile are studied u
nder forward and reversed flow conditions. The profile chord is cut by
3, 6, and 9 percent of the chord at the sharp trailing edge end and t
he performances of these profiles are compared. It is found that with
increase in length of cutting the lift coefficient increases in forwar
d direction and decreases in reverse direction of flow. Cutting off th
e sharp trailing edge improves the lift-drag characteristics in forwar
d mode and deteriorates in the reverse mode.