Why Fast Jets Have Swept Wings: Boldmethod Live

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Күн бұрын

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Why do fast aircraft have swept wings? We explain all the details. Tune in to learn more and ask questions.
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Пікірлер: 31

@joaomarcos6394 2 жыл бұрын

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

🥴

@bigdogboos1 4 жыл бұрын

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

@jaxav8r 3 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: kzfaq.info/get/bejne/q82Afbx7kqivm4k.html

@mdshaheenalam4737 3 жыл бұрын

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

@gbanderas2479 5 жыл бұрын

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

@hansrachmadi9584 4 жыл бұрын

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!

@amadoudiarra3686 4 жыл бұрын

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

@lejetjockmd11 2 жыл бұрын

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.

@janinemarish4419 Жыл бұрын

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

@jalenbutler5567 Жыл бұрын

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

@iamra_n3189 2 жыл бұрын

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

@chrisarya3253 4 жыл бұрын

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

@IdisWaidis 4 жыл бұрын

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

@JavierRamirez-ki1bi 3 жыл бұрын

You guys are amazing doing this

@linmingjet9260 3 жыл бұрын

Best ever! Thank you so much.

@someguy1746 3 жыл бұрын

Really good video!

@muhammadsaid3934 3 жыл бұрын

Amazing and spectacular

@nkkkn8320 4 жыл бұрын

perfect, thanks a lot

@bahaaali6226 5 жыл бұрын

Thanks Alex Excellent

@Boldmethod 5 жыл бұрын

Thanks for watching!

@crazyaces9586 Жыл бұрын

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. 👍👍

@alexanderioakim3467 4 жыл бұрын

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

@chrisarya3253 4 жыл бұрын

Please do a live on weather

@chrisberg4952 5 жыл бұрын

The Best

@saulsavelis575 4 жыл бұрын

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

@diegom8 Жыл бұрын

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 2 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