Lift vs Coefficient of Lift. What's the difference?

[@vogahl34]

The clarity of these videos is inspiring. Thank you

[@flightclubonline]

You are so welcome

[@romeomike62]

The best aviation knowledge channel on KZbin. Please don't stop putting out such amazing content :D

[@shreejiplacements2799]

You are right. Very true

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Thank you so much! These videos have got me through college!

[@flightclubonline]

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[@abeeconstable7877]

Fantastic, finally an aeronautical presentation that is thorough and professional.

[@flightclubonline]

Wow, thanks!

[@robertg5393]

Your videos are THE BEST. THANK YOU.

[@flightclubonline]

Wow, thank you!

[@johnclarke1045]

I have finished my ATPL exams. But occasionally I review concepts from time to time. Your graphics, combined with articulate delivery of information often makes me wonder why you are not in the ATPL game as a content provider. You would definitely have my thumbs up. Tone and speech delivery all to perfection and quality graphics as well. I only commented to offer that piece. Keep up the great work no matter the direction you take. Many benefit from the quality material. Fair play. 👍

[@flightclubonline]

Congratulations on finishing your ATPL exams. Thank you so much for such positive feedback. Stay tuned for future developments ;)

[@willm6598]

One of the best explanations I have ever seen, if you guys made content for universities to explain aerosapce concepts for their courses, you would make a killing. There is no amount I wouldn't pay to learn my courses this way

[@flightclubonline]

Wow, thank you so much. Maybe I’ll do that one day:)

[@PhantomP63]

Even at my regional airline, sometimes channels like Boldmethod and University of North Dakota (UND)’s videos are referenced as training aids. Your work would be a shoe-in!

[@MGBGamer]

The Intros and Graphics just keep getting better!

[@petersevcik8412]

Beauty of voice, presentation and visual experience. Thank you!

[@flightclubonline]

Thank you too!

[@danchow9222]

Excellent Animation! Thank you

[@ironchicken7240]

I finally understand coefficient of lift. Thanks a lot. I'll stick around for more content

[@KLee-yj7vs]

This is very clear and concise! Thank you! 😄

[@flightclubonline]

Thank you so much!

[@dhonnytheodoro5754]

Finally understood! Thanks !

[@flightclubonline]

Great!

[@arashborzoei]

The best of best explanation. Thank you so much. 🙏🏻☺️

[@flightclubonline]

You're very welcome!

[@jmarcosvieira9415]

I love this channel so much, why can't all the groundschools use materials like these?

[@flightclubonline]

Thank you so much for such positive feedback.

[@praveens9014]

A very good explanation. Coeff of lift is a non dimensional parameter. Engineering requires extensive use of non dimensional parameters so as to obtain meaningful information and quantifying data.

[@flightclubonline]

Much appreciated.

[@windshearahead7012]

I learned more from this channel, than 6 months of ground school lessons

[@sufysprojects2689]

Fantastic video!!! Very clear and concise!

[@flightclubonline]

Thank you!

[@superstardafunk]

LOVE your videos!

[@flightclubonline]

Thank you!!

[@hercu278]

Absolutely great explanation. Thank you

[@veeravignesh4525]

very good explanation

[@hmabboud]

The perfect explaination!

[@ManojKumar-bv9hh]

Even though I am a lot younger for understanding you even made me understand

[@mkaya4]

What a great explanation!

[@flightclubonline]

Glad you liked it

[@dann5480]

Excellent video

[@flightclubonline]

Thank you very much!

[@bunyaminaktas804]

Good explanation and presantation

[@StrsAmbrg]

When doing this CL test, will the aircraft body (the fuselage) also included in the test? Or the fuselage is constant but we control the cordline with flap and slat?

[@icojb25]

Actually, lift coefficient also takes into account other effects not explicitly specified in the lift equation, including compressibility, viscous effects / shear stress effects etc ... basically all the extra detailed stuff people fight about in terms of "what is lift / how is lift created" (i.e. is it "bernoulli" ie dynamic pressure effects, what about coanda too etc). All the other little bits included in the equations of motion which we dont explicitly specify in the equation for lift are bundled up into Cl ...

[@pk7549]

Compressabily, viscosity and shear effects are predominant in drag effects.

[@TheOdizeo]

What "surface area" is used to calculate the Cl? I am assuming it would be different from the area used to calculate the Cd...

[@slevinshafel9395]

2:11 How measure LIFT? Because only i see lines. Surface of entire plane or just the surface wich are inside the tunel? What if the density change? on the ground is 1080hPA and at 10km is 380hPA. I need more details on it. Thank you.

[@brianbonnell8495]

I’ve been describing this accurately but poorly to my students for a year. Thank you lol

[@flightlevelview2115]

Hey Flight Club, do you plan on making a Coffin Corner video?

[@flightclubonline]

Great idea! Thank you.

[@sourabhjain9075]

Which refrence books do you use ?

[@Mikester4411]

Wait, so in order to calculate lift you need the lift coefficient, but in order to calculate the lift coefficient, you need to know the lift? I'm trying to code the physics for wingsuiting in my game but I'm stumped by this, am I missing something obvious here?

[@pk7549]

CL is dimenshionless. It has no value. You don't exactly calculate it.

[@fookinsmooth4722]

Wow, Thank you

[@flightclubonline]

You're welcome!

[@beaunoya4794]

I'm assuming wing shape is referring to its cross-section shape and not its profile(?)

[@zahidk333]

Awesome

[@autopick1902]

whats the music in the backgroud

[@maxagafonov3670]

👍

[@dallascowboy2221]

I’m closer to understanding CL after this video

[@Lamusicainfinita]

CL = AOA

[@alfaisalgtr]

ok