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Question: If \( \alpha \) of a body is given by \( \alpha \left( \theta \right) = 3\theta - 2\left( {\dfrac{{r...

If α\alpha of a body is given by α(θ)=3θ2(rads2)\alpha \left( \theta \right) = 3\theta - 2\left( {\dfrac{{rad}}{{{s^2}}}} \right) . Find ω\omega of a body after it covered 3 rad, if it was at rest at the start of the circular motion.
(A) 11 rad/s\sqrt {11} {\text{ rad/s}}
(B) 12 rad/s\sqrt {12} {\text{ rad/s}}
(C) 15 rad/s\sqrt {15} {\text{ rad/s}}
(D) 14 rad/s\sqrt {14} {\text{ rad/s}}

Explanation

Solution

The angular acceleration can be defined as the rate of change of the angular velocity ω\omega with respect to time. The statement “it was at rest at the start of circular motion” signifies that at the angular displacement θ\theta or time tt equal to zero angular velocity is equal to zero too.

Formula used: In this solution we will be using the following formulae;
dω=αdtd\omega = \alpha dt where ω\omega is the instantaneous angular velocity of a body, α\alpha is the instantaneous angular acceleration, and tt is time.
ω=dθdt\omega = \dfrac{{d\theta }}{{dt}} where θ\theta is angular displacement.

Complete Step-by-Step solution:
To solve the above question, we note that we are given the equation of the angular acceleration of a body with respect to its angular displacement.
The equation is
α(θ)=3θ2(rads2)\alpha \left( \theta \right) = 3\theta - 2\left( {\dfrac{{rad}}{{{s^2}}}} \right)
We also note that we can write that
dω=αdtd\omega = \alpha dt where ω\omega is the instantaneous angular velocity of a body, α\alpha is the instantaneous angular acceleration, and tt is time.
From mathematical principles, this can be written as
dωdθdt=αdθd\omega \dfrac{{d\theta }}{{dt}} = \alpha d\theta
But we know that
ω=dθdt\omega = \dfrac{{d\theta }}{{dt}} where θ\theta is angular displacement.
Hence, we have
ωdω=αdθ\omega d\omega = \alpha d\theta
Integrating both sides, we have that
ω22=αdθ\dfrac{{{\omega ^2}}}{2} = \int {\alpha d\theta }
Hence, inserting the given equation, we get
ω22=(3θ2)dθ\dfrac{{{\omega ^2}}}{2} = \int {\left( {3\theta - 2} \right)d\theta }
ω22=32θ22θ+C\Rightarrow \dfrac{{{\omega ^2}}}{2} = \dfrac{3}{2}{\theta ^2} - 2\theta + C
Now, we were told that at the beginning of the motion, hence,
We have
ω2=2(32θ22θ)=3θ24θ{\omega ^2} = 2\left( {\dfrac{3}{2}{\theta ^2} - 2\theta } \right) = 3{\theta ^2} - 4\theta
Now, at angular displacement of 3 rad, we have
ω2=3(3)24(3)=15{\omega ^2} = 3{\left( 3 \right)^2} - 4\left( 3 \right) = 15
ω=15rad/s\Rightarrow \omega = \sqrt {15} rad/s
Hence, the correct option is C.

Note:
For clarity, we have simply prove the validity of the equation dωdθdt=αdθd\omega \dfrac{{d\theta }}{{dt}} = \alpha d\theta by cancelling out common terms and multiplying both sides by dtdt in which we get dω=αdtd\omega = \alpha dt .
Also, the constant CC is equal to zero in the equation ω22=32θ22θ+C\dfrac{{{\omega ^2}}}{2} = \dfrac{3}{2}{\theta ^2} - 2\theta + C because, if we write make θ\theta and ω\omega zero, we have
(0)2=32(0)22(0)+C\dfrac{{\left( 0 \right)}}{2} = \dfrac{3}{2}{\left( 0 \right)^2} - 2\left( 0 \right) + C
C=0\Rightarrow C = 0.