how do engineer determine the location of the centre of gravity for an air craft which they are designing
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Answered by
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well if you see at the basics its the same method that is used to find center of mass of an object but very complex calculations take place
yukesh1:
bro answer properly plz
if you wanna go in details
the other guy is explaining see his answer for an easy refrence
Answered by
1
The first step is divided the sections
The make calculations for there c.g.
And the
For ex
We have 3 sections
So we will calculate there cg separately
Find cg along x and y or any reference axis
And I.e.
X bar=a1x1+a2x2+a3x3/sum of all the areas of section
a1=area of 1 section
x1= distance of the cg from reference axis
Similarly a2, a3 and x1, x2
Similarly make calculation for y(bar)
And finally we get the cg points of complete lamina
The make calculations for there c.g.
And the
For ex
We have 3 sections
So we will calculate there cg separately
Find cg along x and y or any reference axis
And I.e.
X bar=a1x1+a2x2+a3x3/sum of all the areas of section
a1=area of 1 section
x1= distance of the cg from reference axis
Similarly a2, a3 and x1, x2
Similarly make calculation for y(bar)
And finally we get the cg points of complete lamina
link me to what?
are you by any chance in 11th...???
a uniform meter scale can be balanced
no9th
....
well so you don't need to know about the method of finding canter of gravity
you won't probably understand
sorry mistyped it was center
and it can be balanced at a point where its center of mass is located
or you could say geometric center
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