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Question

ABC is a plane lamina of the shape of an equilateral triangle. D, E are mid-points of AB, AC and G is the centroid of the lamina. The moment of inertia of the lamina about an axis passing through G and perpendicular to the plane ABC is I0. If the ADE is removed. The moment of inertia of the remaining part about the same axis is NI016 where N is an integer. The value of N is


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Solution

Let, mass of triangular lamina =m,
length of side =l,
Then the moment of inertia of the lamina about an axis passing through centroid G perpendicular to the plane is,

I0ml2
I0=kml2 [k=shape factor]
Let us divide the given lamina ABC into four equal lamina as shown,


Let the moment of inertia of (DEF)=I1 about G
I1(m4)(l2)2ml216 I1=I016
Let IADE=IBDF=IEFC=I2
3I2+I1=I03I2+I016=I0 I2=5I016
Hence, moment of inertia of DECB i.e., after removal part ADE
I=2I2+I1=2(5I016)+(I016)=11I016=NI016
Therefore, value of N=11

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