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A ballerina begins a tour jet (Figure a) with angular speed Ӭiand a rotational inertia consisting of two parts : role="math" localid="1661005078220" Ileg= 1.44 kg.m2 for her leg extended outward at angle θ= 90.0°to her body and Itrunk= 0.660 kg.m2 for the rest of her body (primarily her trunk). Near her maximum height she holds both legs at angle30.0°to her body and has angular speedӬf(Figure b). Assuming that Ihas not changed, what is the ratioӬfӬi ?

(a) Initial phase of a tour jet: large rotational inertia and small angular speed. (b) Later phase: smaller rotational inertia and larger angular speed.

Short Answer

Expert verified

Ratio of final to initial angular velocities is Ó¬fÓ¬i=1.52.

Step by step solution

01

Step 1: Given

Ileg=1.44kg.m2Itrunk=0.660kg.m2

02

Determining the concept

Calculate initial rotational inertia when leg extending at 900and final rotational inertia when leg extending at300. Then, apply law of conservation of momentum to find the ratio of final to initial angular velocities. According tothe conservation of momentum, momentum of a system is constant if no external forces are acting on the system.

Formula are as follow:

  1. Initial angular momentum = Final angular momentum
  2. role="math" localid="1661005530030" Ii=Itrunk+Ileg

Where,Itrunkis moment of inertia of trunk andIlegis moment of inertia of leg

03

Determining the ratio of final to initial angular velocities

Initial rotational inertia when both leg extending 900outward,

Ii=Itrunk+IlegIi=0.660+1.44=2.10kg.m2

Final rotational inertia when both leg extending300 outward,

If=Itrunk+IeffIf=Itrunk+2Ilegsin2(θ)

The factor 2sin2θarises from the fact that there are two legs and each one of them is stretched at an angle 30°. So, effective length from the axis of rotation would be,

leff=Lײõ¾±²ÔθIeff=mleff2=mL2sin2(θ)Ieff=2mL2sin2(θ)Ieff=2Ilegsin2(θ)

If=0.660+2×1.44sin2(30)=1.38kg.m2

Now, according to law of conservation of momentum,

Li=LfIiÓ¬i=IfÓ¬f

Hence,

Ó¬fÓ¬i=IiIf=2.101.38=1.52

Hence, ratio of final to initial angular velocities is Ó¬fÓ¬i=1.52.

Therefore, the total rotational inertia of the system can be found. Using the law of conservation of momentum, ratio of angular velocities can be found.

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