One of the best videos for education , very simple and good explanation

A small correction. A fluid tends to move from a high pressure region to a low pressure region, for instance the wing tip vortex. So, the adverse pressure gradient is when the fluid moves to a relatively higher pressure (dp/dx > 0), contrary to what was stated at 3:05.

That video was great ! I was struggling with the boundary layer a lot and I understand way better now Thanks !!

Thank you Sir for your valuable and excellent explanation. It really got my concepts cleared !!! Please#KEEP UP THE GOOD WORK !!! 😃👍🍫

your video helped me lot thanks for sharing knowledge i am doing PHD

Really, today I got know about the vortex generators,Thank you sir.

I needed some clarification on this topic. Very informative, thank you!

Very well explained and great graphics; thanks for posting.

thankyou. best video on this topic! clearly understood everything!

Great and nice explanatory information. Very great.

This very helped me alot thanks

Always the best explanation

Thank u very mucch for the best explanation

Thank you so much!

📝 Summary of Key Points: 📌 The boundary layer is a thin layer of fluid that forms on the surface of an object as it moves through a fluid, caused by friction between the fluid and the surface. 🧐 There are two types of boundary layers: laminar and turbulent. Laminar boundary layers reduce skin friction drag and improve aerodynamic efficiency, while turbulent boundary layers are thicker and cause more skin friction drag but can withstand adverse pressure gradients and prevent flow separation. 🚀 Understanding the boundary layer is crucial for optimizing the aerodynamic efficiency of objects like aircraft wings and sports equipment. 💡 Additional Insights and Observations: 💬 "The boundary layer only forms in a viscous fluid." 📊 Laminar boundary layers reduce skin friction drag, while turbulent boundary layers cause more skin friction drag but can withstand adverse pressure gradients. 🌐 References and Sources: The video does not mention any specific references or sources. 📣 Concluding Remarks: The boundary layer is a significant concept in fluid dynamics that affects the movement of objects through fluids. Understanding the different types of boundary layers and their impact on drag and flow separation is crucial for optimizing the aerodynamic efficiency of various objects. Made by Talkbud

Super good explained

Where is start from boundary layer seperation leading edge or trailing edge

Hello, what I do not understand is why you said laminar boundary layer is to reduce the drag at first, but then gave an example of golf and tennis ball that holes on them were made to create turbulent flow to reduce drag. I feel lost on the concept that its is turbulent or laminar flow which can reduce the drag. Hope you can answer me , thank you !

Great video🙌🏼

Nice video 👍

At 1:32 , why does the speed of the air particles gradually increase?

thanks for this

I always thought that a turbulent boundary layer causes early air separation, a bad thing.

Skill issue. ( this is revenge for Simon from the 8 weens

The authors have two wrong scientific approaches: researching the creation of Lift force and Low pressure at upper side of the wing, relative to the ground surface and Earth. I explain the aerodynamic cavitation and existence of Lee side aerocavern, and creation of Aerodynamic force. Low pressure creates force normal to the cord (contact surface), and it name is "aerodynamic force" because is made from the air (aero) in motion (dynamic), or wind relative to the wing (object).