Why do you have planes in diagrams facing into us when your explaining left and right it’s actually backwards and I think maybe easier to understand if plane facing forward and you can see ailerons moving up and down? What do you think ?
Most of what you say is correct but there are some major flaws. Adverse yaw only occurs when you roll into a bank. That is when you balance it with rudder. Once you are in the bank your aileron is neutral and there is no more adverse yaw. You maintain your nose attitude and away you go. The only rudder needed in the turn is if needed enough to balance any engine effects like slipstream. There is no rudder needed for the turn. What makes the plane turn is bank. Hope this helps.
The point is you don’t say that . I said it to correct your video. No rudder is needed in a turn because there is no adverse yaw in the turn. It happens only on the roll into a Turn.
The video is about adverse yaw and therefore the whole time I talk is assumed to be during moments of adverse yaw. Sorry for the confusion. Thanks for the comment.
Yes induced drag decreases with velocity you are correct. My saying that was meant to be for specific aircraft and aircraft configuration. The more lift an aircraft produces because it is either heavier or has bigger wings, the more induced drag it will create. But you are correct that for a specific aircraft as it increases its airspeed the induced drag decreases. Hopefully I didn’t say it increases with speed. If I did, sorry
Why do you have planes in diagrams facing into us when your explaining left and right it’s actually backwards and I think maybe easier to understand if plane facing forward and you can see ailerons moving up and down?
What do you think ?
@@CaptLouSantaBarbara maybe! I guess it depends on the person
Most of what you say is correct but there are some major flaws. Adverse yaw only occurs when you roll into a bank. That is when you balance it with rudder. Once you are in the bank your aileron is neutral and there is no more adverse yaw. You maintain your nose attitude and away you go. The only rudder needed in the turn is if needed enough to balance any engine effects like slipstream. There is no rudder needed for the turn. What makes the plane turn is bank. Hope this helps.
Where exactly do I say that? Lol
The point is you don’t say that . I said it to correct your video. No rudder is needed in a turn because there is no adverse yaw in the turn. It happens only on the roll into a Turn.
The video is about adverse yaw and therefore the whole time I talk is assumed to be during moments of adverse yaw. Sorry for the confusion. Thanks for the comment.
Why do you say that more lift equal more induced drag, if you see the graphs is the opposite
Yes induced drag decreases with velocity you are correct. My saying that was meant to be for specific aircraft and aircraft configuration. The more lift an aircraft produces because it is either heavier or has bigger wings, the more induced drag it will create. But you are correct that for a specific aircraft as it increases its airspeed the induced drag decreases. Hopefully I didn’t say it increases with speed. If I did, sorry