Sir at 05:18 - 'pitching moment will be zero' or 'it will not change' is the correct statement. About ac, pitching moment doesn't change with AoA, so, it should remain constant n not zero I believe sir
How does the plane detect the change in alpha ? Does it get unstable ? And how is this fixed ? Like what helps detect the change ? Is a gyroscope or similar device used to detect the change which will lead to fix the change ?
Sir but why are you not considering pitching moment about ac(shift lift force from cop)? In that case we can move ac ahead of cg in flying wheel too. Plus it will have +ve M0 at zero aoa.
Awesome explanation with very good examples. Thank you very much
thanks you, sir....i always had doubts on stability but now i understand!!!
Sir at 05:18 - 'pitching moment will be zero' or 'it will not change' is the correct statement. About ac, pitching moment doesn't change with AoA, so, it should remain constant n not zero I believe sir
Great explanation sir thank you 🙂
Awesome, thank you very much.
Thank you sir....very nicely explained.
NICE CLASS SIR
How does the plane detect the change in alpha ? Does it get unstable ? And how is this fixed ? Like what helps detect the change ? Is a gyroscope or similar device used to detect the change which will lead to fix the change ?
😂 Love and hate relationship
best explanation
Sir but why are you not considering pitching moment about ac(shift lift force from cop)? In that case we can move ac ahead of cg in flying wheel too. Plus it will have +ve M0 at zero aoa.
Thank you so much
Sir, can you explain static stability for negative alpha?
In that case delta(cl) will be acting downwards and the aircraft will have a nose up moment about c.g....statically stable condition
Yes sai nivedh vallala u are correct and the resulting moment will also be in the negative direction hence nose up movement
Don’t love 💖 too much 😂
2
bohot bekar bore kardie bhai