The moment of inertia of a lamina S : x 2 + y 2 = 1 , ( 0 ≤ z ≤ h ) of unit density about the line z = 2 h in the x z p l a n e can be represented by π ⋅ h ( a h 2 + b ) , where g cd ( a , b ) = 1 .
Find: a + b .
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I was amazed when I first learnt about the Parallel Axis Theorem , and how it could greatly simplifies calculating moment of inertia through an arbitrary axis.
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Yeah, it's great. My general approach is either to use the PAT or represent it as a double (or triple) integral and compute it numerically.
Two points on line z = 2 h in the x z p l a n e are:
A : ( 0 , 0 , 2 h ) a n d B : ( 1 , 0 , 2 h ) ⟹
Line A B i s : x = t , y = 0 , z = 2 h , where the direction numbers of line A B a r e u = i + 0 j + 0 k
Let P : ( x , y , z ) be a point not on line A B and v = x i + y j + ( z − 2 h ) k be vector from point A t o P .
The distance d from point P to line A B is: d = ∣ u ∣ ∣ u X v ∣
u X v = 0 i + − ( z − 2 h ) j + y k a n d ∣ u ∣ 2 = 1 ⟹
d 2 = ( z − 2 h ) 2 + y 2
for x 2 + y 2 = 1 , ( 0 < = z < = h ) ⟹ r ( u , z ) = c o s ( u ) i + s i n ( u ) j + z k where ( 0 < = u < = 2 π ) and ( 0 < = z < = h ) ⟹
r u = − s i n ( u ) i + c o s ( u ) j + 0 k , and r z = 0 i + 0 j + k ⟹
r u X r z = c o s ( u ) i + s i n ( u ) j + 0 k ⟹ ∣ r u X r z ∣ = 1
⟹ d A = ∣ r u X r z ∣ d u d z = d u d z
and, d 2 = ( z − 2 h ) 2 + y 2 = z 2 − h z + 4 h 2 + s i n 2 ( u ) ⟹
∫ ∫ S d 2 d A = ∫ 0 h ∫ 0 2 π ( z 2 − h z + 4 h 2 + s i n 2 ( u ) ) d u d z =
∫ 0 h ( ( z 2 − h z + 4 h 2 ) ∗ u + 2 1 ∗ ( u − 2 1 s i n ( 2 u ) ) ) ∣ 0 2 π d z =
2 π ∗ ∫ 0 h z 2 − h z + 4 h 2 + 2 1 d z = 2 π ∗ ( 3 z 3 − 2 h ∗ z 2 + 4 h 2 ∗ z + 2 z ) ∣ 0 h = 2 π ( 1 2 h 3 + 2 h )
= 6 π ∗ h ∗ ( h 2 + 6 ) = π ∗ h ( 6 h 2 + 1 ) = π ∗ h ( a h 2 + b ) ⟹ a + b = 7 .
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