ATPL Principles of Flight - Class 6: Wing Design.

preview_player
Показать описание
ATPL Principles of Flight - Class 6: Wing Design.
---------------------------------------------------------------------------------------------------------------------------

Welcome to Class 6 in the ATPL Principles of Flight series.

The way a wing is designed is based off trying to find the perfect balance between correct lift with minimal drag. There are other choices to be made depending on the type of flying intended such as gliding or in fast jets.

In this class we will look at the reasons for some of these choices and also the basic components of a wing used by designers to describe the shape.

Sign up to Airhead ATPL question bank with a 10% discount with this link:

---------------------------------------------------------------------------------------------------------------------------
Aiming to assist with ATPL theory exams and the ground school aspect of ATPL training. Including helpful tips for studying and to use in the exam.

LIKE and SUB so you don't miss future videos.
Рекомендации по теме
Комментарии
Автор

Hi. Your videos are very helpful but could you pls set volume of background music a little lower? It would be easier to listen your narration this way.

ddddfffify
Автор

Quite confused here. When looking at the rectangular wing, there is clearly a higher amount of lift being produced at the root of the wing (as you can see from the lift distribution), but you are saying we have strong wing tip vortices because we have more downwash at the tips...

However with the swept + tapered wing, from the lift distribution, there is much lower lift at the root than the tip, but you are saying downwash is greatest at the root? Why is this? Looking at the lift distribution, there is much greater lift at the tips, which should equal greater downwash at the tips too, no?

Aceperformance
Автор

at 11:45 for rectangular wing, you said there'a still a large amount of lift produced at the tips, but your graph shows CL gradually goes to 0 at wingtip... why?

Kelvin-edce
Автор

What a stupid idea with a background music!!!

DukaSerega
Автор

Thanks for making these videos public! Is the area thats derived by multiplying span and chord length the same area that used to calculate the lift as the S in the formula?

OxibanCraft
Автор

Thank you these are great really clear videos

debs
Автор

I'm a new student is very beneficial

mehliselosigauke
Автор

"if you die you go up to heaven" that was wild

guillemgomezpuig
Автор

The music makes me sleepy 😅, I can’t concentrate

amiraamore
Автор

do you mind if I ask : is Delta wing intentionally omitted, is it going to be explained later on?

thanks a lot by the way, your videos are really helpful, you really managed to explain complicated topics in a very effective manner.

lucacagnazzi