Комментарии:
*looks at padpilot*: i don't want to play with you anymore
ОтветитьSHORT & PRECISE ❤
ОтветитьExcellent simple and clear explanation. Rare!
ОтветитьGreat explanation. Thanks
ОтветитьWhy Angle of Incidence doesn’t change with flap extension?
ОтветитьBeat go hard
ОтветитьThank you for short and clear explanation!
😊
Huh?
Ответитьthank you very much for your videos .
ОтветитьThe explanation is very good. The unwanted-backround-music extremely annoying.
ОтветитьIf 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?
ОтветитьAngle 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.
ОтветитьI am also the new viewer and new subscriber to your channel. Keep on helping us like this, thank you.
ОтветитьCan you pls tell me "is angle of attack is always greater than angle of incidence?"
ОтветитьPerfect explanation thank you!
Ответитьan angle of incidence exists only in case of a cambered wing profile though right?
ОтветитьBeautifully demonstrated
ОтветитьThankyou for this, it really helped a lot. May you always follow GOD's guidance. Keep safe
ОтветитьI just can’t handle the accent!
Ответить👍👍👍 no comment 👍👍👍
ОтветитьIf I'm understanding this correctly, it seems as though the angle of incidence is mainly based on the construction of the plane.
ОтветитьHello 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.
Ответитьsome 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.
ОтветитьWow that was an amazing explanation! Thank you!!
Ответитьabsolutely clear explanation. I got it instantly from the visualisation rather than from the tedious textbook
ОтветитьThank you! The way my ground instructor explained it didn't make that much sense to me!
ОтветитьThis is the best channel, thanks
ОтветитьTHANK YOU!!!
ОтветитьI still don't understand what angle of incidence is for a helicopter.
ОтветитьSimply the best explaination! Thank you.
ОтветитьGreat explanation
ОтветитьThank you for your videos, which app do you use for animation
Thanks again
the wing appears to be twisted down at them tip ???
ОтветитьWhat's the name of that song??
ОтветитьI have never fly an aircraft. So, how do actually AOA is being changed in flight?
Ответитьi am a new viewer and i m loving it
Ответитьso angle of incidence is included in the angle of attack?
ОтветитьIncredibly resourceful channel, thanks.
ОтветитьGreat video. Just subscribed!
ОтветитьSo for a rotor blade, such as in a wind farm, the angle of incidence and angle of attack are equal
ОтветитьThank you very much. I will subscribe.
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