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Ron Natalie wrote:
Matt Whiting wrote: A vertical stabilizer does not provide any lateral force unless there is some degree of slip or skid. Precisely! Now you are beginning to understand. As soon as uncoordinated flight occurs (skid or slip) the vertical stab deflects the aircraft back into the coordinated flight. It does sounds like you are beginning to understand! With use of the rudder, you can enter and exit a turn and maintain coordination at all times. Without rudder and depending on the fin alone, you will be in and out of coordinated flight as you enter and exit the turn. The degree of departure from coordinated flight maybe be large or small depending on the specific airplane and the rate at which you enter and halt the turn, but without using the rudder, you will NOT be coordinated at all times. That's it's job! It is the primary job to provide the primary aerodynamic forces to keep the airplane coordinated. In coordinated flight, it is just along for the ride. Yep, and as soon as something deflects the aircraft from coordinate flight, it generates a force to correct it. Yes, which is precisely what I said at the start. You have to enter uncoordinated flight for the fin to work. With proper rudder use, you can remain coordinated at all times (if you are good enough). Many airplanes will oscillate slight in the yaw axis for this reason. And they oscillate in pitch, and they oscillate in roll. This is one of the fundamental modes of stability. Yes, and that is one reason you have control surfaces, to stop these oscillations or prevent them. It takes a very large vertical stab to keep the excursions small enough to not be detectable, especially in a longer fuselage airplane. The rudder can provide a side force in anticipation of a slip or skid and thus maintain coordinated flight and never allow the slip or skid to develop in the first place. Are you trying to tell me that you sit there and tweak the rudders during flight continually to damp yaw oscillations? Don't think anybody finds that fun. The few airplanes where it is a persistant problem have autopilots that do that, but for most it's unnecessary in normal flight regimes. No, that is what yaw dampers are for. But, yes, I use the rudder and ailerons and elevator to damp oscillations caused by turbulence when they exceed a certain threshold. No sense in waiting through several oscillations when you have the controls to stop it now. |
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