Understanding STALL: Across an Aircraft WING and In An Aircraft ENGINE

[@sadayarkoil]

Thank you so much for all your educational videos. What we get free are gems that we have to pay a fortune. God bless you and this channel. I do share your videos as much as I can.

[@JxJAVIATION]

Thank you and You are Welcome! :)

[@salmankadirshaikh9945]

Thanks a lot jxj aviation because of your helpful video 😢

[@JxJAVIATION]

Thank you! Check out my other videos as well!

[@王王思远]

AOA is the angle between the wing chord line and relative wind ,not the horizon.

[@anesukafesu7875]

Understanding this what made stalls finally make sense to me. Relative wind is not necessarily horizontal, it's opposite to the flight path. When the wings point in a very different direction from relative wind, the won't flow smoothly and won't generate lift. Thus results in a stall.

[@milanjeevanraj6500]

beautifully explained...thanks a lot

[@JxJAVIATION]

You're most welcome

[@bongD1950]

Much appreciation for your videos, they're indeed helpful

[@JxJAVIATION]

Glad you like them!

[@dennissmall132]

Educational

[@JxJAVIATION]

thank you! and Welcome! Check out my other videos as well!

[@RayleneCawood]

Now understand that Whale Tubercles greatly increase the angle of attack range of a wing before stall and look them up already! :)

[@JxJAVIATION]

cool

[@bullitanaconda]

Sorry to correct you but at 0:30 sec you are confusing pitch angle with angle of attack A stall does not occur when a high pitch angle is obtained A stall occurs when a critical angle of attack is obtained ….15 to 20 degrees for most aircrafts, big difference between the two You could be in a 45 degree angle of pitch and still maintain zero degrees of angle of attack As long as the aircraft is fliying in the same direction where the chord line is pointing at, the angle of attack will remain the same. The angle of attack increases when the relative airflow is not aligned with the the chord line The angle of attack is determined by the chord line and the relative airflow not by the horizontal axes line as you suggested at 1:37, at this time you are confused with the angle of incidence In other words if you are in a pitch nose up attitude but flying in a straight leveled flight, you have increased the angle of attack If you have the plane pitched nose up attitude and the plane is flying in the same direction as where the nose is pointing there is no angle of attack being increased, the airflow is aligned with the chord line. Flaps play a major role on the angle of attack as well . the more flaps are deployed de greater the angle of attack, which generates more lift but you will reach the critical angle of attack quicker the plane will stall at a lower nose attitude with the flaps deployed but again only if you are moving in a different direction of where the chord line is pointing at. you can also reache the critical angle of attack in a roll attitude if using the elevator to turn.

[@JxJAVIATION]

Yes. Should have been more specific in the explanation! Thank you for the clarification!

[@RAHULKUMAR-wm9wk]

Thnku thnku so much.! ❤🙏

[@JxJAVIATION]

You are Welcome!

[@saeedalwahabi]

Thank you

[@JxJAVIATION]

You're welcome!

[@ashusingh7553]

Ap airlines se ho..i mean aviation industry se?

[@ambigaisri7214]

Super ❤

[@JxJAVIATION]

Thank you. Check out my other videos as well!

[@OmSaiSwarupSetty]

Is it possible both Wing and Engine stall will be occured at the same time? If yes, how to overcome?

[@JxJAVIATION]

There is a small possibility that both may occur at the same time. To overcome it the best way is to increase thrust and reduce the angle of attack.

[@OmSaiSwarupSetty]

@@JxJAVIATION Thank you😊, By the way loving your content, No course on online academy or youtube dont have the content like you, I am blessed with your channel😇

[@JxJAVIATION]

@@OmSaiSwarupSetty Thank You! Please do share and check out my other videos as well.

[@sabaalenezi2606]

Ur the best!!!

[@JxJAVIATION]

Thank you so much! You made my day!

[@alexandersmith3751]

What’s the difference between engine stall and engine surge?

[@JxJAVIATION]

Engine surge or increase in shaft speed could be one of the consequences of an engine stall.

[@mp4338]

Thank a lot for video and explication. The english terms are difficults for me, for example DRAG, TRUSTH, etc. I need dictionary. A lot of abrevations. For a first time of course I have problem to keep a lot of avionic terms.

[@JxJAVIATION]

Glad it was helpful! Keep Learning!

[@jyotichaurasia8025]

If the stall is on wing before the root what will happen

[@JxJAVIATION]

I did not understand the question. Can you please elaborate!

[@tech4you159]

Angle of attack for cri cri egal how much

[@JxJAVIATION]

around 14 deg

[@tech4you159]

@@JxJAVIATION thank you