Lift, Coefficient of Lift

This video consists of the following :
Why is lift generated?
Lift Coefficient
Lift formula
Coefficient of Lift and Angle of Attack Graph
Effect of high lift devices
Cases of the Lift Equation
Stalling angle
TAS, IAS variation

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Cheers and Happy landings! :)

[karthikeyanbalasubramanian]

The best video on Aerodynamics till date ! Kudos ! Clear accent and lucid explanation ! Keep it up !

[epicghost]

This is very good. I’m basic when it comes to physics of any form but you make it quite simplistic and able for persons such as myself to understand. Thank you so much!!!

[himanshuahuja]

till i saw this video i had so many confusions...thanku so much for making it so clear and easy to understand...
Respect
Regards

[engrhaseeb]

SIR U R GREAT U TEACH IS AXM AND EASY M REALY MOTIVATED WITH UR WAY OF TEACHING YOU SIR

[Gryronaut]

I really enjoy your videos and attitude towards teaching. Good job.

[rishirajchugh]

your videos are really helpful. great job. in your lift and coefficient of lift video u said at 40000 ft density is 1/4. So to mantain lift TAS should be 4 times. I think it should be twice as TAS is a square function.

[Hussain-byct]

Nice video sir u explained perfectly all concept related to lift now I remember❤️💓tnx u sir for ur best vdo

[gensyed]

Thank you for the refresher course. The last bit there, I think you meant to say High Altitude density and not High density altitude.

[EvaGolubinska]

Thank you for these vids. Very helpful!!

[poh]

I will be uploading in few days. Need some time to make these videos. Been busy. :)

[Realfoodreallife]

Very nice video...I m able to understand all the terms clearly...above all my basics are improving...So, Thank u so much for making such informative videos...and keep doing the same in future as well 😊👍🏼

[lucille]

Thank you very much, so easy to understand.

[smilenhustle]

Great work, great content keep up the great work!

[shamee]

superb.. i have one request..can u tell me about TAS and IAS in detail.. plzz

[rchauhan]

11:40 you said half rho v square is constant, if v square increases, rho decreases, but isn't that a decrease in altitude then ?

[surajmahendraramraj]

thank you soo much this lesson really helped me.

[nathanielho]

Can you upload a video about the pressure settings? I'm a bit confused about it. Thank you in advance

[karenlee]

May I ask if the +ve sign at the leading edge refers to the dynamic pressure? Im confused with the 16 degrees AOA. Does it mean that the aerofoil stalls because of a reverse pressure differential or because the downwash is not completed with the flow stream?

Also, could you please explain how does Bernuelli's principle of total pressure (unchanged) = static + dynamic apply between AOA 14 degrees and 16 degrees. I really dont get it.

[girishkv]

Best video.. very informative.. 👍👍

How lift is generated?? Is there any detailed video on this from you sir?

[FuadPhenomenon]

What is the unit for L? And, in order for the equation to work, can we out the AOA value in degrees?