Great, clear and concise as usual but I’ve been taught in my flight school that the up going wing produces more lift as well as induced drag than the down going wing, because the aileron on the up going wing deflects downward and increases the camber of that wing hence creating more lift and also induced drag because it has a higher AOA than the down- going wing, hence differential ailerons and frise ailerons are designed on ailerons to reduce the downward deflection of the up-going wing’s aileron and increase drag on the upward deflected aileron of the down-going wing respectively. Please correct me if I’m wrong, thank you.
Absolutely unique videos on the web. Complex things in a simple language. Short videos that is cover whole concepts. Keep going. I am CFI and I learned a lot from your videos on the way, even some of the stuff I already know I like to watch just because the way you explain it giving me a tips how to explain complex concepts to a student
@@flightclubonline this phenomenon is actually very similar to the dihedral effect on low wing aircraft. But the key difference between autorotation and dihedral effect is that the dihedral effect has the relative wind flowing over the fuselage and hitting on the wing that’s going down but in this case it’s just mainly to do with the angle of attack differences
Thanks for explanation. However, i have trouble with how dropping wing has higher angle of attack with respect to upgoing one. Could you please explain it or is there any explained video?
I don't know where you got that from. I've been building and flying model planes since the 1950's and even flew full scale planes for a few years. I have never heard of anything like this. When a plane is in a spin, it does do what's called autorotation, but it's more like what a falling maple seed does. Also, dihedral in the wing is what makes a plane self-level. As one side goes higher, it produces less lift and comes back down.
Spot on mate, this is just a bullshit term for a spin. Typical examiners are always creating some other way of describing the same phenomena we’ve been experiencing for decades.
The best presentation of flying. Perhaps zoomed on the specific object to highlight clearer.
I love your teaching style!
Thank you! 😃
Great, clear and concise as usual but I’ve been taught in my flight school that the up going wing produces more lift as well as induced drag than the down going wing, because the aileron on the up going wing deflects downward and increases the camber of that wing hence creating more lift and also induced drag because it has a higher AOA than the down- going wing, hence differential ailerons and frise ailerons are designed on ailerons to reduce the downward deflection of the up-going wing’s aileron and increase drag on the upward deflected aileron of the down-going wing respectively. Please correct me if I’m wrong, thank you.
Absolutely unique videos on the web. Complex things in a simple language. Short videos that is cover whole concepts. Keep going. I am CFI and I learned a lot from your videos on the way, even some of the stuff I already know I like to watch just because the way you explain it giving me a tips how to explain complex concepts to a student
Thanks a ton
Your videos lessons are inspirational. Once again many thanks for your hard work.
😊
So nice of you
Amazing explanation with the diagram at the end!
Glad you liked it!
@@flightclubonline this phenomenon is actually very similar to the dihedral effect on low wing aircraft. But the key difference between autorotation and dihedral effect is that the dihedral effect has the relative wind flowing over the fuselage and hitting on the wing that’s going down but in this case it’s just mainly to do with the angle of attack differences
Very short Video but excellent explained.... 👍👍.... Thank you So much for such great videos
Thank you for your feedback.
Great video. Thank you
Glad you liked it!
More and more vids needed...
Cool vid...
Thanks so much. More coming.
Thanks for explanation. However, i have trouble with how dropping wing has higher angle of attack with respect to upgoing one. Could you please explain it or is there any explained video?
Hi there. We talk about this concept in our 'adverse yaw' video. See if this helps: ua-cam.com/video/D9cIof2O6Mc/v-deo.html
@@flightclubonline Thank you again i will watch this
@@umutsari5853 Dihedral is what helps keep the wing level.
Thank you.
No worries!
I don't know where you got that from. I've been building and flying model planes since the 1950's and even flew full scale planes for a few years. I have never heard of anything like this. When a plane is in a spin, it does do what's called autorotation, but it's more like what a falling maple seed does. Also, dihedral in the wing is what makes a plane self-level. As one side goes higher, it produces less lift and comes back down.
Spot on mate, this is just a bullshit term for a spin. Typical examiners are always creating some other way of describing the same phenomena we’ve been experiencing for decades.
Do more it's very useful great ❤️ and do on propeller.🇮🇳
Thank you! Will do!
How rotation contributes to metal failure in aging airplanes??
Thanks.
Welcome!
I don't see a difference between a spin and an autorotation. Where's the difference between them?
the autorotation is the condition when the aircraft automaticaly yaw and roll and occurs when the spin is developing