Reynolds number explained.

preview_player
Показать описание
Welcome to another lesson in the "Introduction to Aerodynamics" series!
In this video I explain the concept and the formula of the Reynolds number, one of the most important parameters in aerodynamics.

If this video was helpful for you, subscribe to my channel to be notified when the next lesson comes out!

Connect with me:
Рекомендации по теме
Комментарии
Автор

Thank you for taking the time to do the explanation.
Re<2100=laminar and Re>4200=turbulent ONLY applies in closed channels such as pipes, not for external flow such as airfoils.

FranzBond
Автор

The tranistion point is incorrect in this video for a wing, 2100 to 4000 is for flow in a pipe

For a wing, without inducing it by changing the AoA, it is about 500, 000, eg the variable is velocity only.

To induce it by stalling the wing the transition point is about 50, 000.

Using the transition value for a pipe and applying it to a wing is common mistake people make when dealing with Reynolds numbers.

LeoHL
Автор

Thank you! I finally understood the Reynolds number :)

claramelb
Автор

Very well explained. I am from electrical background and still able to understand every bit of this video. Thanks!!!

balajilakshminarayan
Автор

help me a lot to solve my Fluid Mechanic project, Thanks so much. Love from Malaysia

mohamadfahrulradzi
Автор

Excellent Aliya mam I understood it's👍

charchitgaur
Автор

Thank you for video. Love from pakistan. Finally understand renold number

vibinhigh_
Автор

You're awesome. Thanks for the clear and concise content.

TheMrMEEEEE
Автор

Good job. If you could make a video explaining how to scale airfoils up and down to maintain RE, that would be good. Theres a burst of RC Airplanes being designed right now and we are all wanting to properly access existing airfoils, which will involve scaling them down.

reeceengineering
Автор

Did you say the Reynolds numbers will be same for the wind tunnel testing and the real size plan ??

LindoMtsweni
Автор

hey, Aliya I have a question, please. if a steel pipe with a diameter 0.02 m is used to deliver jet fuel from the tank to the engine of an aircraft. The jet fuel has a density of 900 kg/m3 and kinematic
viscosity 5×10-6 m2/s. If the engine burns 1000 kg of jet fuel per hour.
what would be the Reynolds number of the flow?

Sondus-yuhl
Автор

Thank you for teaching Me this Reynolds number!!!

fernandofreitasalvesdelima
Автор

thank you for your wonderful lecture and appearance

백승원-ez
Автор

Airflow that is attached to a wing can be laminar or turbulent.

andrecarvalho
Автор

Hi

I'm a bit confused, I understand that the effect of low Reynolds number on an airfoil is increased drag and decreased lift. Which is more desirable, a high or a low Reynolds number for a wing airfoil?

R_Alexander
Автор

Basically your English is very easy to understand from India
Your English is better and so good

manjpoooegx
Автор

im doing a wind tunnel report for airfoil 0012
to find reynolds number, i have to use the chord length?

Fiendnat
Автор

Question...maybe its a dumb one but here goes...If Laminar flow is Re<2100 and Turbulent is Re>4000, what happened between 2100 and 4000?

marccretten
Автор

VSE (Vid Scoring Equation): ECF (Eye Candy Factor) * EV (Educational Value) = VSE, and in this example 10*10 = perfect score of 100

heydonray
Автор

Reynolds number is fluid so we will define it for gases because we some time deal with gases so how will elect it flow type
?

mazharameerpg