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.
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.
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.
2:06, 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.
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
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
sorry but i cant understand it. CG i know and the explanation is not so helpfull in this video. I expect learn about Cp but i cant get it from this video.
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.
That's great! You are welcome! Do Keep watching and please share as well!
@@JxJAVIATIONMost definitely 👍
Amazing how two points can control the entire stability of an aircraft. Excellent review
Thanks a lot!
My curiosity leads me to this video.
Watching while boarding IndiGo to Delhi.
Cheers for easy explanation 🍻
Thank you!
Thanks for your videos! They’re truly excellent (: my only recommendation is organizing the playlists into the 13 topics!!
You are welcome! Will keep your recommendation for the future uploads!
Excellent, thanks for posting.
Thanks for watching!
Very well explained. Thanks alot!
Welcome! Do check out my other videos as well!
This was very helpful! Thank you so much!!!!!!!!
Glad it was helpful! Check out my other videos as well!
Great explanation of the relation CG and CP have.
Thank you!
Amazing explaination 🥺
Glad you liked it
Thank you to make this videos
It's my pleasure
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.
Thank you for sharing!
Excellent video
Thank you!
Very informative Thank You for Posting
Thank you! Check out my other video as well!
Wish you’d have discussed tail down force and how it affects stability as well
have created a video on the stabilities on an aircraft.
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.
The rotation is about the center of gravity. Here the moment is zero. The CoL is where the resultant lift acts.
great vid ! thanks a lot !
You are welcome!
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?
I love your videos!!!
Thank You! Check out my other videos as well!
Outstanding!
Thank you! Check out my other video as well!
2:18 if the AoA decreases, lift increases and CP moves aft?
didnt get that
very informative
Glad it was helpful!
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.
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
Thank you! I have made a few videos on Turbofan and Turboprop engines. Do check it out! and inform me if anything specific required!!
@@JxJAVIATIONplz upload a video on stalling
Sir I am your big fan.. Kindly make a video on fadec and idg system.. Please
Sure!
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.
Thanks
Thank you! Do check out my other videos as well!
Whether centre of pressure is always in airfoil
The reference for CP is always taken on the 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
sorry but i cant understand it. CG i know and the explanation is not so helpfull in this video. I expect learn about Cp but i cant get it from this video.
oh! You may ask your doubts here for clarification!
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.
Lol European or American didn't invent the plane
Aww man~
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