Re: Why do helicopters \"chop\"?
</font><font color="blue" class="small">( Well now isn't this interesting There was some science behind my question. I would assume most of the "chop" was from the doppler shift in blades moving toward/away from a distant observer. In the vehicle, the blades aren't moving towards/away but rather around which is more steady state. If the chop is still present in the vehicle there must be another element going on? Something to do with the variation in pitch as the rotor revolves? Someone else mentioned effects over the tail versus over open air elsewhere? )</font>
You're getting closer. /forums/images/graemlins/ooo.gif
I guess it is time to throw in my 2 cents. You are right in your observation about the doppler effect. The compression of the sound waves as an object is approaching will amplify the perceptipon of the "chop." As the helicopter moves away from you, the increased spacing between sound waves, caused by the moving acoustical source, force the doppler shift in the opposite direction and the chop appears to be decreased. While riding in the helicopter the chop is constant or at least the chop due to doppler is constant, since anyone who has ridden is helicopter knows the chop isn't constant.
Now for the second theory. The chop is not caused by blades hits turbulence or vortices from the other blade. The blades generate lift, thus pushing the air and it's wake downward. Even for a helicopter in hover, each blade hits clear air continously. There is some excellent visualization of this effect in high load, high humidity cases; you can see the vortices spiraling around the helicopter downward to the ground. These vortices are long lived, and just as in a commercial airplanes can cause real problems. Encountering wake was the problem with the V-22 that has crashed several times. Due to pivoting it's own props and descending too quickly, the V-22 encoutered it's own wake.
So what's the answer? The chop is caused by the the blade tips reaching super-sonic speeds. The sonic boom that is created is your chop. The sonic boom is a discontinuity in the fluid flow, which is basically a steep pressure wave. As you have started to deduce, change in pitch of the blades causes a change in chop. The blade pitch controls how much lift is generated. For supersonic flow, varying blade pitch changes the size & shape of the sonic boom and thus changing the intensity of the chop.
Okay, maybe that's a buck 50's worth. /forums/images/graemlins/wink.gif