For more than two weeks I've been trying to understand the principles teached in this video in order to understand the difference between vortex generators and wing fences. I started with books, then articles on the internet and finally I found this amazing class. Thank you so much to all bold method team, you are awesome!!!

@user-lj5fd6gk5p

Жыл бұрын

🥴

Best video ever! The EASA students can feel the importance before ATPL exams

This is the clearest instructor i've ever seen. great bar to reach for

@jaxav8r

2 жыл бұрын

Guys your explanation about how shockwaves for above wing don’t really make a lot of sense. Your notion that the airflow moves from the leading edge to the trailing edge … but it gets backed up because it’s moving too fast it .., doesn’t make a lot of sense. Look at the explanation offered by the military explanation of shockwave formation. Their explanation is completely opposite of yours. They explained that the pressure waves are building up from the trailing edge and they get blocked up as they try to move forward. That seems a lot more intuitive, doesn’t it? Look at the 2:50 mark on this video: kzread.info/dash/bejne/p5uErLuDXaWxm7g.html

Great stuff! Helps a lot short before PoF ATPL exam. Thanks for sharing it!

I usually don’t comment often but I just have to say you manage to create a new level of knowledge. Informative, interesting and whatnot. Thank you!

you guys are Amazing!!! Pleasee pleasee continue doing these episodes they really help and are extremely educational! Thanks guys!

Excellent presentation, truly enjoyed. To be more precise, M# = TAS/LSS. LSS meaning the local speed of sound. LSS (in KT) = 38.94 V Absolute Temperature (K) LSS (in KT) = 38.94 V°C + 273. (It’s not a V it’s a square root, can’t seem to replicate). Keep up the nice work.

Excellent video on jets swept wings and absolutely top notch explanations!!

Thank you SO much for this content. This helped me breeze through my airline interview. You are truly an exceptional instructor

Studying for the EASA ATPL Principles of Flight syllabus...so this lecture was a fantastic supplement. Great job guys, subbed!

Awesome videos, very informative and detailed. Please continue making these

Best ever! Thank you so much.

perfect, thanks a lot

Awesome presentation, very helpful. Thank you very much Sir!

You guys are amazing doing this

Amazing and spectacular

Really good video!

Thanks Alex Excellent

@Boldmethod

4 жыл бұрын

Thanks for watching!

Nice vid. In regards to the 747, they have leading edge 'Krüger flaps', not slats.

Thanks late to the party 🥳...I'm a long time H.p. amateur rocket's and fly rc jets,planes. Understand the vortex,slats,exc. 👍👍

Please do a live on weather

The Best

The illustration showing the shockwave over the wing is incorrect. A shockwave is formed at 1.0 not 1.05 or anything above 1.0, but right at 1.0. Other than that, it is a very good video.

@kirillbolshacov5590

Ай бұрын

The shockwave is formed when the airflow slows down to below M 1.0, not speeds up to 1.0 This presentation is correct, as it's shown in between 1.05 and .95, showing the formation just as it falls under 1.0

have you stalled a transport category aircraft

temperature increases the velocity of each individual molecule, thus and the sound speed is increased

Let’s Gooooooo

I don't see any prandtl on these wings... Good