Man, your physical example with the ruler, string, and water bottle makes the abstract real. Great demo. I wish all aviation subjects were simple like that.
Thank you for making these videos! In aviation, it's all about the "WHY's", and this answered all of my questions in relation to Forward and AFT CG characteristics.
Can we say that critical angle of attack is lower with forward cg because stall speed is higher? On the other hand cl max is higher because we need to produce more lift?
@@piquecuriosity no critical angle of attack is constant, it does not change. with forward cg you’re going to be at a higher AoA at any given airspeed so you’re closer to that critical angle
@@maxcfi7718Thanks for replying. I think we are on the same page. We are taught that for example when you put flaps down stall speed is reduced, cl max is higher and critical angle of attack is reduced but i guess Cr AoA can not be lowered in any way. What they mean is you will reach the C AoA earlier. So, in our F Cg scenario because we need more lift we should increase AoA and we will reach C AoA earlier. I think what you mentioned by "you are closer that critical angle " is the same with i have meant.
@@maxcfi7718 Great 👍. Thanks for sharing knowledge. I would like to see content about flight planning and performance also if it is possible. You are a great teacher 🖐️
with fwd cg u said downward tendency inc bcz of inc in distance btw cp and cg but at the same time distance btw cg and tail down force also inc na and therefore dont u think nose up tendence will be inc without inc td force but just this distance ?
i see what you’re saying, however while the distance between the cg and tail does increase, this was already a greater distance to begin with and so the increase is proportionally smaller.. hope that makes sense
Man, your physical example with the ruler, string, and water bottle makes the abstract real. Great demo. I wish all aviation subjects were simple like that.
wow the effects of forward and aft CG has been something i was struggling to remember but this was so clear and helped it click! thank you!
This is one of the most underrated video ever!
Thank you for this! This is the best video I've seen thus far explaining the cg effects on an airplane.
Thank you for making these videos! In aviation, it's all about the "WHY's", and this answered all of my questions in relation to Forward and AFT CG characteristics.
Prob the best video out there on this topic I’ve seen
Very clear illustration, thank you. 🙏🏽
Great video! Thanks for taking the time to make it! I have shown to my students.
love to hear that!
MAN!!!!! GREAT VIDEO!!!!!! YOU'RE AN AMAZING TEACHER ! PLEASE KEEP MAKING VIDEOA !!!!!!!!!!!!!!!
Excellent explanation of this concept. This one has been hard for me to understand so thank you for explaining it clearly and visually.
glad to help!
FANTASTIC explanation!! Thank you so much for sharing!!
Great video.
Great video, just what I needed. Thanks
This is great! Thank you. I just started out
amazing video - you explained it well! thank you!!
Thank you! the visuals help a ton
Hi, sorry im not to familiar with the term cruising faster or slower what does that mean for the range and endurance of the plane?
great channel.
Amazing stuff
Bravo, never seen it put like this.
Thanks for this. Excellent explanation
Great explanation
Amazing video
this is a great explanaition! thanks!
Great explanation 👏
Thank you very much for the video!!
Thanks very much for this video , Help me understand weight and balance effects for my PPL
I really like this teaching ! I hope you have more vid’s !!!
Can we say that critical angle of attack is lower with forward cg because stall speed is higher? On the other hand cl max is higher because we need to produce more lift?
@@piquecuriosity no critical angle of attack is constant, it does not change. with forward cg you’re going to be at a higher AoA at any given airspeed so you’re closer to that critical angle
@@maxcfi7718Thanks for replying. I think we are on the same page. We are taught that for example when you put flaps down stall speed is reduced, cl max is higher and critical angle of attack is reduced but i guess Cr AoA can not be lowered in any way. What they mean is you will reach the C AoA earlier.
So, in our F Cg scenario because we need more lift we should increase AoA and we will reach C AoA earlier. I think what you mentioned by "you are closer that critical angle " is the same with i have meant.
@@piquecuriosity yes exactly that’s right. critical AoA is fixed, you’ll just start out closer to it and so reach it sooner as your airspeed decreases
@@maxcfi7718 Great 👍. Thanks for sharing knowledge. I would like to see content about flight planning and performance also if it is possible. You are a great teacher 🖐️
Thank you sir for this video!
Nicely explained
with fwd cg u said downward tendency inc bcz of inc in distance btw cp and cg but at the same time distance btw cg and tail down force also inc na and therefore dont u think nose up tendence will be inc without inc td force but just this distance ?
i see what you’re saying, however while the distance between the cg and tail does increase, this was already a greater distance to begin with and so the increase is proportionally smaller.. hope that makes sense
Thank you.
This was the last video I watched before taking the par. I passed!!!!!!!
congratulations!
soo helpful thank you
Are you an instructor?
yep!
thanks a lot