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. 👍
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
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!
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.
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.
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?
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 ...
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?
The best aviation knowledge channel on TH-cam. Please don't stop putting out such amazing content :D
You are right. Very true
Fantastic, finally an aeronautical presentation that is thorough and professional.
Wow, thanks!
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. 👍
Congratulations on finishing your ATPL exams. Thank you so much for such positive feedback. Stay tuned for future developments ;)
The clarity of these videos is inspiring. Thank you
You are so welcome
Thank you so much! These videos have got me through college!
You are so welcome!
Your videos are THE BEST. THANK YOU.
Wow, thank you!
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
Wow, thank you so much. Maybe I’ll do that one day:)
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!
How clearly picturized. Hats Off
This is very clear and concise! Thank you! 😄
Thank you so much!
Beauty of voice, presentation and visual experience. Thank you!
Thank you too!
Excellent Animation! Thank you
Finally understood! Thanks !
Great!
The Intros and Graphics just keep getting better!
I finally understand coefficient of lift. Thanks a lot. I'll stick around for more content
very good explanation
The best of best explanation. Thank you so much. 🙏🏻☺️
You're very welcome!
Fantastic video!!! Very clear and concise!
Thank you!
LOVE your videos!
Thank you!!
The perfect explaination!
Absolutely great explanation. Thank you
I love this channel so much, why can't all the groundschools use materials like these?
Thank you so much for such positive feedback.
Even though I am a lot younger for understanding you even made me understand
What a great explanation!
Glad you liked it
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.
Much appreciated.
I learned more from this channel, than 6 months of ground school lessons
Good explanation and presantation
Excellent video
Thank you very much!
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.
Hey Flight Club, do you plan on making a Coffin Corner video?
Great idea! Thank you.
Awesome
Which refrence books do you use ?
I’ve been describing this accurately but poorly to my students for a year. Thank you lol
Wow, Thank you
You're welcome!
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?
What "surface area" is used to calculate the Cl? I am assuming it would be different from the area used to calculate the Cd...
👍
I'm assuming wing shape is referring to its cross-section shape and not its profile(?)
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 ...
Compressabily, viscosity and shear effects are predominant in drag effects.
whats the music in the backgroud
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?
CL is dimenshionless. It has no value. You don't exactly calculate it.
I’m closer to understanding CL after this video
CL = AOA
ok