Angle of incidence vs angle of attack.

*looks at padpilot*: i don't want to play with you anymore

SHORT & PRECISE ❤

Excellent simple and clear explanation. Rare!

Great explanation. Thanks

Why Angle of Incidence doesn’t change with flap extension?

Beat go hard

Thank you for short and clear explanation!
😊

Huh?

thank you very much for your videos .

The explanation is very good. The unwanted-backround-music extremely annoying.

If the AOI is the angle between the chord line and the longitudinal axis, then isn't it correct to say that the pilot CAN change the AOI in flight? Lowering the flaps changes the chord line, so why would this not have an impact on the AOI?

Angle of incidence = between longitudinal axis and chrod line
AOA = between relative wind and chrod line

Kindly tell me
"Angle of incidence" is the angle between "chord of aerofoil" and "longitudinal axis" of aircraft. And you said it remains same.
When the flaps are lowered, chord line of aerofoil changes and hence should "angle of incidence" change ???

Sorry for bad English

A better video would have been pitch angle vs angle of attack.

I am also the new viewer and new subscriber to your channel. Keep on helping us like this, thank you.

Can you pls tell me "is angle of attack is always greater than angle of incidence?"

Perfect explanation thank you!

an angle of incidence exists only in case of a cambered wing profile though right?

Beautifully demonstrated

Thankyou for this, it really helped a lot. May you always follow GOD's guidance. Keep safe

I just can’t handle the accent!

👍👍👍 no comment 👍👍👍

If I'm understanding this correctly, it seems as though the angle of incidence is mainly based on the construction of the plane.

Hello Pilots,
Do I understand it right that,
Stall will happen when you have a large angle of attack at relative low speed?
But
if, with the Same Angle of Attack, the speed is much higher, then stall
won't happen. Right? And the plane will climb up of course. Right?

If not right, Then how come that fighter jets and other acrobatic planes can climb straight vertically?
I suppose this is because of their high speed, which provides enough lift, no matter in what direction or angle they move.
So why can't normal plans in a critical angle of attack give full thrust to gain more lift?
The
air is the same everywhere in the sky. Why behaves the air different if
we want to fly in an angle which is not parallel to the horizon?

at :41, WRONG !!!!!!! if the the thrust Line remains the Same (which it does), the aoa does NOT change. the only exception is during gliding flight.

some very late info. at :34, 'relative airflow' SHOULD be explained. it is the Result of the Angle at which a wing is Pulled/pushed through the air by the prop; aka the thrust LINE.

Wow that was an amazing explanation! Thank you!!

absolutely clear explanation. I got it instantly from the visualisation rather than from the tedious textbook

Thank you! The way my ground instructor explained it didn't make that much sense to me!

This is the best channel, thanks

THANK YOU!!!

I still don't understand what angle of incidence is for a helicopter.

Simply the best explaination! Thank you.

Great explanation

Thank you for your videos, which app do you use for animation
Thanks again

the wing appears to be twisted down at them tip ???

What's the name of that song??

I have never fly an aircraft. So, how do actually AOA is being changed in flight?

i am a new viewer and i m loving it

so angle of incidence is included in the angle of attack?

Incredibly resourceful channel, thanks.

Great video. Just subscribed!

So for a rotor blade, such as in a wind farm, the angle of incidence and angle of attack are equal

Thank you very much. I will subscribe.