Jurgen M
Something like this?c=centerline,rudder constant speedjbriggs444 said:2 is indeed a tough sell. With the right parameters, it might be achieved, but I will not attempt to make a plausibility argument here.
1 is easy. Any asymmetry will do. And we have an obvious one.
At the end of the forward stroke, as the foil is brought to rest, this slows the entrained fluid mass. This results in a forward thrust.
At the beginning of the backward stroke, as the foil is sped back up toward the center, this accelerates the entrained fluid mass. This results in a forward thrust.
The symmetry that was expected has the pressure gradient equal and opposite throughout the corresponding portions of the two strokes. But "forward" is not equal and opposite to "forward".
M=middle,rudder constant speed
D=point where rudder start deccelerate
A=point where rudder stops accelerate
S=point where rudder complety stops
H=high pressure
L=low pressure
red arrow= resultant force perpendicular to rudder surface