Let lamina S : x 2 + y 2 = 1 , 0 ≤ z ≤ h , and axis A : the line x = x 0 + a t , y = y 0 + b t , z = z 0 + c t .
Find a general formula for the moment of inertia I of the lamina S of unit density about A , then let x 0 = y 0 = z 0 = 0 and a = b = c .
If the moment of inertia I can be represented as I = β α π h ( λ + h 2 ) , where g c f ( α , β , λ ) = 1 .
Find: α + β + λ
Note: My intention here is to have the person find a general formula for I given lamina S : x 2 + y 2 = 1 , 0 ≤ z ≤ h of unit density, and axis A : the line x = x 0 + a t , y = y 0 + b t , z = z 0 + c t , of course you need not do so, and just proceed using x 0 = y 0 = z 0 = 0 and a = b = c .
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The inertia tensor of a cylindrical shell of radius 1 and height h about its centre of mass is I = ⎝ ⎛ 1 2 1 m ( 6 + h 2 ) 0 0 0 1 2 1 m ( 6 + h 2 ) 0 0 0 m ⎠ ⎞ and so the moment of inertia of the cylinder about the axis through the centre of mass in the direction of the unit vector v = ⎝ ⎛ a b c ⎠ ⎞ is I 0 = v T I v = 1 2 1 m ( 6 + h 2 ) ( a 2 + b 2 ) + m c 2 = 6 1 π h ( 6 + h 2 ) ( a 2 + b 2 ) + 2 π h c 2 since the mass of the cylinder is m = 2 π h .
The distance from the origin 0 to the above axis through the centre of mass, with equation r = λ v + a = λ v + ⎝ ⎛ 0 0 2 1 h ⎠ ⎞ λ ∈ R is ∣ a ∣ 2 − ( a ⋅ v ) 2 = 2 1 h 1 − c 2 and hence the moment of inertia of the cylinder about the axis in the direction of the unit vector v that passes through the origin is I = I 0 + 4 1 m h 2 ( 1 − c 2 ) = I 0 + 2 1 π h 3 ( 1 − c 2 ) With a = b = c = 3 1 we have I = 9 1 π h ( 6 + h 2 ) + 3 2 π h + 3 1 π h 3 = 3 4 π h + 9 4 π h 3 = 9 4 π h ( 3 + h 2 ) making the answer 1 6 .
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Let B : ( x , y , z ) be any point not on the given line and choose the points 0 : ( x 0 , y 0 , z 0 ) and A : ( x 0 + a , y 0 + b , z 0 + c ) on the given line.
The distance from point B to the given line is d = ∣ O A ∣ ∣ O B X O A ∣
0 A = a i + b j + c k
0 B = ( x − x 0 ) i + ( y − y 0 ) j + ( z − z 0 ) k
O B X O A = ( c ( y − y 0 ) − b ( z − z 0 ) ) i + ( a ( z − z 0 ) − c ( x − x 0 ) ) j + ( b ( x − x 0 ) − a ( y − y 0 ) ) k
⟹ d 2 = a 2 + b 2 + c 2 ( c ( y − y 0 ) − b ( z − z 0 ) ) 2 + ( a ( z − z 0 ) − c ( x − x 0 ) ) 2 + ( b ( x − x 0 ) − a ( y − y 0 ) ) 2
r ( θ , z ) = c o s ( θ ) i + s i n ( θ ) j + z k where ( 0 < = θ < = 2 π ) and ( 0 < = z < = h ) ⟹
∂ θ ∂ r = − s i n ( θ ) i + c o s ( θ ) j + 0 k , and ∂ z ∂ r = 0 i + 0 j + k ⟹
N = ∂ θ ∂ r X ∂ z ∂ r = c o s ( θ ) i + s i n ( θ ) j + 0 k ⟹ ∣ N ∣ = 1 ⟹
d 2 = a 2 + b 2 + c 2 ( c ( s i n θ − y 0 ) − b ( z − z 0 ) ) 2 + ( a ( z − z 0 ) − c ( c o s θ − x 0 ) ) 2 + ( b ( c o s θ − x 0 ) − a ( s i n θ − y 0 ) ) 2
Simplifying we obtain:
Let f ( z ) = 2 ( y 0 c 2 + b c ( z − z 0 ) + y 0 a 2 − a b x 0 )
g ( z ) = 2 ( x 0 c 2 + a c ( z − z 0 ) + + x 0 b 2 − a b y 0 )
m ( z ) = ( a 2 + b 2 ) ( z − z 0 ) 2 + 2 c ( b y 0 + a x 0 ) ( z − z 0 )
K = x 0 2 ( b 2 + c 2 ) + y 0 2 ( a 2 + c 2 ) − 2 a b x 0 y 0 + 2 a 2 + b 2 + c 2
d 2 ( θ , z ) = a 2 + b 2 + c 2 ( 2 b 2 − a 2 ) c o s ( 2 θ ) − f ( z ) s i n θ − g ( z ) c o s θ − 2 a b s i n θ c o s θ + m ( z ) + K
I = ∫ 0 h ∫ 0 2 π d 2 ( θ , z ) d θ d z = ,
a 2 + b 2 + c 2 1 ∗ ∫ 0 h ( ( 4 b 2 − a 2 ) s i n ( 2 θ ) + f ( z ) c o s θ − g ( z ) s i n θ − a b ( s i n θ ) 2 + ( m ( z ) + K ) θ ) ∣ 0 2 π d z =
a 2 + b 2 + c 2 2 π ∫ 0 h m ( z ) + K d z =
a 2 + b 2 + c 2 2 π ( ( 3 a 2 + b 2 ) ( z − z 0 ) 3 + c ( b y 0 + a x 0 ) ( z − z 0 ) 2 + K z ) ∣ 0 h =
a 2 + b 2 + c 2 2 π ( ( 3 a 2 + b 2 ) ( h − z 0 ) 3 + c ( b y 0 + a x 0 ) ( h − z 0 ) 2 + K h + ( 3 a 2 + b 2 ) z 0 3 − c ( b y 0 + a x 0 ) z 0 2 ) ,
where K = x 0 2 ( b 2 + c 2 ) + y 0 2 ( a 2 + c 2 ) − 2 a b x 0 y 0 + 2 a 2 + b 2 + c 2
Now letting x 0 = y 0 = z 0 = 0 and a = b = c we obtain:
I = 9 4 π h ( 3 + h 2 ) = β α π h ( λ + h 2 )
⟹ α + β + λ = 1 6
Again, my intention was to have the person find a general formula for I given lamina S : x 2 + y 2 = 1 , 0 ≤ z ≤ h of unit density, and axis A : the line x = x 0 + a t , y = y 0 + b t , z = z 0 + c t .