A 0.84-lb collar with center of mass at G and a uniform cylindrical horizontal a
ID: 2991708 • Letter: A
Question
Explanation / Answer
(a) Moment of inertia of arm I = WaL2/3 = 1.3*12/3 = 0.433 lb-ft2
Initial moment of inertia of system H0 = (I+mcd2)0 = (0.433+0.84*0.472)*1.42 = 0.879 lb-ft2/s
We have d2r/dt2 = H02r/(I+mcr2)2
and (d2r/dt2) dr = (dr/dt)(d/dr(dr/dt))
So, H02r/(I+mcr2)2 dr = (dr/dt)(d(dr/dt))
Integrating left hand side over r and RHS over dr/dt we have,
-H02/(2mc(I+mcr2)) + C1 = (dr/dt)2/2 + C2
Taking the integral from r = d to r = L,
-H02/(2mc(I+mcL2))+H02/(2mc(I+mcd2)) = 1/2*((dr/dt)L2 - (dr/dt)d2)
Putting (dr/dt)d = 0
We have the impact speed at A, (dr/dt)L = H0[1/mc(I+mcd2) - 1/mc(I+mcL2)]
= 0.879 * [1/0.84*(0.433+0.84*0.472) - 1/0.84*(0.433+0.84*12)]
= 0.879*(1.9246 - 0.935)
= 0.874 ft/s
(b) Now, at radius r, Moment of inertia of cylindrical collar about z-axis is, Icr = 1/12*mc[3*(rin2 + rout2) + l2] + mcr2
Moment of inertia of the system = I + Icr = 0.433 + 1/12*mc[3*(rin2 + rout2) + l2] + mcr2
This expression is similar to expression in part (a) except for the term 1/12*mc[3*(rin2 + rout2) + l2] = 0.001682
Hence, replacing I by I+0.001682 (=0.4347) in part (a) we get,
So, H0 = (0.4347+0.84*0.472)*1.42 = 0.8807 lb-ft2/s
We have the impact speed at A, (dr/dt)L = H0[1/mc(I+mcd2) - 1/mc(I+mcL2)]
= 0.8807 * [1/0.84*(0.4347+0.84*0.472) - 1/0.84*(0.4347+0.84*12)]
= 0.8807*(1.9195 - 0.9339)
= 0.8012 ft/s
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