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Alpha T depends on the airspeed

Where does Al Bowers fit into all this?

Шлема, ты потерял в своем уравнении одну силу и твоя система сил перестала быть замкнутой , мамкин математик без практики -))) Удали все и переосмысли свои наблюдения .

Thank you!!! Subscribed!

at 9:42 how u multiply by tanphi only specific terms

Is there a full course on flight simulation available somewhere?

Thanks!

Thanks for the video! Can you maybe give a short explanation of why C_L_h has to be > C_L_w? You said that equations can be manipulated to demonstrate that, but I'd like to get just some sort of "understanding" of the reason

thanks

first of all, very accurate, simple, and smooth teaching. this videos was life saving at least for me. home to see more. but would be great if we can have the teaching fills is there way for that?

Is this a method that explained in the paper of Phillips and Snyder 2000?

Hopeless.

Hello thanks for the video. I have one question

Awesome video, I've been trying to find quaternions as they relate to local coordinate systems for planes for a bit now and this really helped. A small note though: that isn't Theta. Even hand written, it's just a O with a - in it. In fancy print, the - might have serifs, but you never write those by hand. It's just a single pen stroke where you start at the left-middle, draw the circle counter-clockwise and then "curve in" to finish on the dash.

you are a genious 😊

Thank you sir.

Amazing!!! Very good approach about the topic.

Hi, when we analyse a inverted airfoil, the circulation will be negative? I have this doubt

But the vertical force is pressure and the axial force is shear

Great Explanation! I was equating P = (T - D - WSinC) * V. Is this wrong? I imagined it as the total power generated during the flight equals the total force on it times its Velocity. total force is (T-D-WSinC). This is based on the simple equation Power = Force * Velocity. So is it wrong to think about it like this?

This is really good! Thanks

That is some very good explanation ! Actually is pretty simple the way you teach it :) Subscribed! Thank you :)

Hi aeroAcademy. i tried joining your newsletter but the email signin seems to be not working?

how can i caculate the maximun pressure from the xfoil data .

Title is misleading. This was a teaser to the online course. Good sales gimmick.

But what causes the oscillation moment to occur? Is it caused by shear and pressure or lift and drag?

great explanation, thank you

How to apply this theory on coefficient of moment, center of pressure, other typical parameters, important for wing design?

A nice shot of knowledge just as introduction w/ epic music lfg

I'm joining!

This is a great video, couldve gonna a little deeper in the mathematics, but otherwise excellence.

can you give me any references where i can study more on these euations

Thank you!

Great! Thank you very much for this tutorual!

Hi I really like your lectures, could please make playlist of these aerodynamics lectures

Thanks man

I think that the Stall limit turing rate was derived wrong?

Excellent explanation, thank you!

For certain circumstances i had to choose EEE. But i want to learn about Aerospace engineering and make Fixed-wing UAV. Sir, would you help me? And suggest me some books so that i can still touch my dream 😅.

Didn't understand anything Back to basics

Is there a playlist so that I can watch fundumentals to aerodynamics in order?

Thank you for this video.

Hi, I dont quite understand what is theta sub f

Your videos are nice but too tough to understand

Please improve your handwriting

I don’t get how all these assumptions are made and people should believe them. Where is the proof that they are valid.

❤

Great video!

wt hell u talking about batch u want battaniye?