Thank you for creating such clear, concise, and high-quality flight training videos. Your explanations are straightforward, the visuals are excellent, and the voiceover is perfect for learning. Your channel stands out as one of the best resources on UA-cam for aviation enthusiasts and professionals alike. Keep up the great work!
Question. Can we place our rudder underneath the fuselage to prevent adverse rudder? Is there any profit of doing it? (Let’s neglect clearense and tail strike)
Wrong, the plane doesn’t roll to the left because the right wing is faster than the left. It’s because the wing has dihedral and yawing the plane causes the relative air to push up on the right wing and down on the left wing. Also, name two airplanes that have the rudder interconnected with the ailerons to prevent “rudder roll”..
I should think yaw-induced roll to the left could be caused by the relative wind "getting under" the right wing (what you say) as well as by the increased airspeed over the right wing (as the video author says.) (To give a more complete picture, I wouldn't merely say it was the right wing's increased airspeed, but also the left wing's decreased speed. That is, I'd say it was the airspeed differential between the right and left wings.) And in this case with swept back wings, it could be due to the effective wingspan differential between the right and left wings. And maybe it could also be due to the reduced wingtip vortex off the right wing and increased vortex off the left wing altering their lift. My question is, which of these phenomena is most responsible for the roll? If the airspeed differential is, than the video author is justified in not mentioning the others in this simple presentation.
@@ezanchi5422 "Relative Wind" is the term I'm familiar with, and it is the airflow produced by an object's motion relative to nearby air. So here the relative air would be the air through which the wing is moving.
Lots of tutorials about adverse yaw, but never seen an explanation of these two counteracting forces of adverse rudder; well done!
Thank you for creating such clear, concise, and high-quality flight training videos. Your explanations are straightforward, the visuals are excellent, and the voiceover is perfect for learning. Your channel stands out as one of the best resources on UA-cam for aviation enthusiasts and professionals alike. Keep up the great work!
Glad it was helpful!
you're clips are amazing ! They should be marketed for everyone to see :) !!
Superb explanation ! 👍👍👍
Thank you 🙂
Lovely explanation
Thanks for liking
Very clear explanation.
5 stars
So nice of you. Thank you very much!
Now I know why whenever I try using the rudder in msfs the plane shakes violently when I stop twisting the joystick
Question. Can we place our rudder underneath the fuselage to prevent adverse rudder? Is there any profit of doing it? (Let’s neglect clearense and tail strike)
How about you state the dihedral is the cause of the roll left
Thanks
Welcome
some fs games have this but when i first seen it i was like is this another bug on this fs
so its normal for planes to do this i see
noice vid btw
Love u people
Wrong, the plane doesn’t roll to the left because the right wing is faster than the left. It’s because the wing has dihedral and yawing the plane causes the relative air to push up on the right wing and down on the left wing. Also, name two airplanes that have the rudder interconnected with the ailerons to prevent “rudder roll”..
What do you mean relative air?
I should think yaw-induced roll to the left could be caused by the relative wind "getting under" the right wing (what you say) as well as by the increased airspeed over the right wing (as the video author says.) (To give a more complete picture, I wouldn't merely say it was the right wing's increased airspeed, but also the left wing's decreased speed. That is, I'd say it was the airspeed differential between the right and left wings.) And in this case with swept back wings, it could be due to the effective wingspan differential between the right and left wings. And maybe it could also be due to the reduced wingtip vortex off the right wing and increased vortex off the left wing altering their lift. My question is, which of these phenomena is most responsible for the roll? If the airspeed differential is, than the video author is justified in not mentioning the others in this simple presentation.
@@ezanchi5422 "Relative Wind" is the term I'm familiar with, and it is the airflow produced by an object's motion relative to nearby air. So here the relative air would be the air through which the wing is moving.
All models of the Convair 240/340/440 had rudder/aileron interconnect cables with springs. I have personally rigged them on Convair 580 conversions.
I wish i knew how to be a Pilot.