Significance of Center of Gravity & Center of Pressure | Effect of CG and CP on Stability 

as an ATPL student i can confidently state that your videos are very helpful, helped me through my PPL and now through my ATPL. Unlike other videos where they talk complicated science, you make things way simpler and easy to understand. Thank you very much.

Amazing how two points can control the entire stability of an aircraft. Excellent review

Thanks for your videos! They’re truly excellent (: my only recommendation is organizing the playlists into the 13 topics!!

Excellent, thanks for posting.

This was very helpful! Thank you so much!!!!!!!!

Very well explained. Thanks alot!

Great explanation of the relation CG and CP have.

Outstanding!

great vid ! thanks a lot !

Very informative Thank You for Posting

Amazing explaination 🥺

Excellent video

Thank you to make this videos

If the center of gravity CG lies ahead, then the aircraft will have positive static stability. If the center of pressure CP is at the exact location, the plane will have neutral static stability, If the CP lies ahead of the CG the aircraft will have negative static stability. The center of gravity is the whole aircraft's weight in a particular location. The center of pressure is all the pressure that lies on an particular location on the plane.

very informative

Hello, can you say do we have a calculation for the center of pressure? How can I calculate the place of the pressure center with my hand?

Thanks

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Your video is very useful to me can u able to make a video on gas turbine engine process and application,...and current engine useage in aircraft. Thankyou

2:46 it is my belief that both cg and cp should occur at/near thirty percent of chord/mac. consequently, this statement should refer to c-m, not cg.

2:06, 2:21 ??? because the amount lift being generated is Also Dependent on other factors, the use of 'amount of lift' as a metric results in a statement that contains NO information.

Hey, I have a question. Are You sure that the control surfaces and their forces rotate around Center of Gravity, not the Center of Lift? I always thought it was the CoL, as it is what keeps an aircraft up in the sky. I would be delivhted if You could explain.

2:18 if the AoA decreases, lift increases and CP moves aft?

Whether centre of pressure is always in airfoil

information :29 it appears that the center of mass (c-m) is indicated in the graphic, NOT the cg*. the c-m of an aircraft is located within the fuselage; at a POINT that lies On the thrust line and vertically aligns with twenty-five percent of chord. 1:20 cg location does have an affect on the effectiveness of aft-located control surfaces. but the statement made here is not really on point. * cg is located AT the wing, and is the span-wise line of balance when an aircraft is FLYING; and the mass of the aircraft is being supported by the main wing. 1:51 cp occurs (at a 'line') ACROSS the span, not at the fuselage.!!! googletranslate

Hello bro.. it's not attitude it's altitude.. u r repeating the same mistake in every video Otherwise ur videos r awesome

There is just something off putting when listening to an Arabic sounding voice explain the mechanics of flight.

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