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#26 | ||
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Member
Join Date: Aug 2012
Location: Boise ID
Posts: 28
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Originally Posted by xmech2k
This is fun! I love talking airplanes!
I'm no expert on the 737. But I got my info from this article, written by a 737 captain. http://usatoday30.usatoday.com/trave...nd-flaps_N.htm I would imagine that the yaw damper does provide some rudder input when turning the airplane. But as I stated in my earlier post, the design of the wing and flight controls (e.g. using flight spoilers to roll the aircraft) can elminate the adverse yaw tendency to the extent that rudder is not needed for a coordinated turn. |
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#27 | ||
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Member
Join Date: Aug 2012
Location: Boise ID
Posts: 28
Thanked 1 Time in 1 Post
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Originally Posted by xmech2k
You are right. However, my earlier post was refering to the rudder input needed when starting the turn to counteract the adverse yaw caused by the aileron deflection. After applying the ailerons and rudder to enter the turn, both controls are neutralized, and elevator back pressure comes into play to maintain pitch attitude. (this could be a climbing, descending, or level turn)
![]() And you are right, ailerons will be (mostly) neutral during a turn. But as you add more and more elevator back pressure, the airplane will tend to shallow its bank or steepen it. (Depends on the wing design) So some aileron is required, as I said, "to maintain the bank angle". ![]() For anyone who wants the real deal on the subject, here's a link: http://en.wikipedia.org/wiki/Adverse_yaw |
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