all these brings back sweet, old memories.... 32 years old, to be precise, when I first learn this stuff before having my first flight in a trainer airplane. Thank you, very good content, now in 2022.

Thank you so much...well explained 👍👍

the things i learnt from this channel fell myself i can fly even tomorrow if i can find a plane :d

Good Day.....on video

G forces are the load factor, increase the Gs in a turn and you increase the wing load and this increases the stall speed.

This is a very good video analysis of AOA and aerodynamics. I like the use of the term "apparent weight". The airplane weighs the same when it is placed on scales while resting on the ground. But if you should place the same airplane on the same scales while flying, the scales will indicate differently at any point in time depending on all the possible factors acting on the airplane at that time. I hesitate to use the word "moment" instead of " time" because the word "moment" has a special meaning for weight and balance purposes, so I'll use "point in time" instead.

Great channel

If​ I​ wonder to​ know how plane​ can fly, We​ need​ to​ understand aerodynamics​ first.​ Thanks, very​ good​ contents.

thank you very much for this video

would the slipstream have similar effect of deflecting the relative airflow on a high wing aircraft?

wow. fluids..

Good video! very logical but I don't understand 'greater ability to generate the lift means that the stalling speed will reduce but the aircraft will stall at a smaller aoa."

When you say that “the aircraft stalls at a smaller angle of attack when using flaps”, does that mean you will stall at less than 16 degrees?

Wow,,,,,,

At

Hello,

Isn’t stall speed irrelevant. It’s about stick position. Stick position indicates AoA. Critical AoA = stall. Heavier planes needs greater AoA at same power. Closer to critical AoA.

The Harry Brown Project

Too fast explained