Understanding a rotational system with centripetal snap, angular jerk, and a third-dimensional tension vector

Question

In a recent experiment in my physics class, we were given the task of finding the experimental rotational moment of inertia in a T-stand with two masses attached to the ends of a certain length. I have drawn a diagram below with the hopes of aiding in the understanding of the problem:

As you can see, I have two point masses hanging off the ends of the T-stand of identical mass M with identical string length S. Mass is distributed uniformly within the T-stand. I am applying a force F tangentially to the edge of the bottom of the T-stand, for which the radius is R.

We were directed as a class to consider that centripetal acceleration as a constant and the tension force as though it only moved in the upward and inward directions. It was then that I made the mistake of pointing out that making these assumptions would not result in accurate data, as we were varying the torque applied to the T-stand. My physics teacher knew that I already had experience with three-dimensional vectors (though very limited) and understood that position (as we had seen it so far) was only the second-degree polynomial of an infinite Taylor series. It was then I was instructed to "go and see if you can figure it out".

The issue of centripetal jerk is apparent when considering the movement of the masses as the F is constant, implying a tangential acceleration. The equation for centripetal acceleration assumes a constant rotational velocity, which this does not have. Thus, we cannot use $a_c = ωr$ (where ω is a constant), but its derivative, $j_c = αr$. Furthermore, the rotational moment of inertia is also increasing with no change in torque applied; thus, angular acceleration is also approaches 0 as time approaches infinity. We cannot even consider centripetal jerk; instead, we must consider centripetal snap: $s_c = ζr$.

This issue would not be too difficult were it not for the three-dimensional tension vector. Since there is a tangential acceleration, there must be a tangential force at the point masses, thus making not only an upward and inward tension force, but also an outward tension force.

Here is what I know so far about the tension vector and the string associated:

$$S^2 = {x_S}^2 + {y_S}^2 + {z_S}^2$$

Where xS, yS, and zS are proportionally related to the force vectors:

$$||vec{F_T}||^2 = ||vec{F_{T_x}}||^2 + ||vec{F_{T_y}}||^2 + ||vec{F_{T_z}}||^2$$

Other misc. knowns (I hope):

$$vec{τ} = vec{F}R = Ivec{α}$$

$$Δvec{τ} = 0$$

$$vec{x_c} = vec{x_{c_0}} + vec{v_{c_0}}t + frac{1}{2}vec{a_{c_0}}t^2 + frac{1}{6}vec{j_{c_0}}t^3 + frac{1}{24}vec{s_c}t^4$$

Note that $vec{x_{c_0}}$, $vec{v_{c_0}}$, and $vec{a_{c_0}}$ all have magnitude of zero. Thus:

$$vec{x_c} = frac{1}{6}vec{j_{c_0}}t^3 + frac{1}{24}vec{s_c}t^4$$

$$frac{d}{dt}vec{v_t} = frac{d}{dt}(vec{ω}r) = vec{a_t} = vec{α}r$$

$$frac{d}{dt}vec{a_t} = frac{d}{dt}(vec{α}r) = vec{j_t} = vec{ζ}r$$

$$vec{ω} = vec{ω}_0 + vec{α}t + frac{1}{2}vec{ζ}t^2$$

$$frac{d}{dt}vec{a_c} = frac{d}{dt}(frac{{vec{v_t}}^2}{r}) = frac{d}{dt}(vec{ω}^2r) = vec{j_c} = 2vec{ω}vec{α}r$$

$$vec{s_c} = 2r(vec{ω}vec{ζ}+vec{α}^2)$$

$$vec{F_c} = Mvec{a_c} = M(vec{j_{c_0}}t+frac{1}{2}vec{s_c}t^2) = M(vec{j_{c_0}}t+r(vec{ω}vec{ζ}+vec{α}^2)t^2)$$

So far, I believe that my interpretation of the fourth-degree polynomial of position. However, relating the three tension vectors in a way that makes any sort of sense becomes my issue.

How I have approached this tension vector so far is by considering the unit vectors relative to the end of the rod, such that $hat{i}$ is always along the rod, $hat{j}$ is pointing towards the tangential movement along the end of the rod, and $hat{k}$ points towards the ground.

I cannot figure out how to relate each vector direction. I know that, as my pointmass is pulled upward and inward by the tension, the radius from the axis of rotation increases for the pointmass, thus increasing the angular acceleration and therefore the tension force along the y-axis is increasing. I know that the tension force along the x-axis also increases, as the x-component distance is becoming larger and therefore increasing the centripetal force. I do not know how to relate the z-axis with other two axes. Here in lies my main issue: relating my tension force components to the variables listed above.

My question is two-fold: are my assumptions about the fourth-degree polynomial of centripetal position and the third-degree polynomial of rotational position equations correct, and how may I relate my tension forces in a way that is theoretically correct?

(full disclosure: I am in AP Physics C with prior AP Calc BC knowledge as well as the beginnings of 3D vector calculus, so if a higher-level calculus is used (I know that tensor calculus might be involved?), please link me to a source that can give me fundamentals of the mathematics necessary)

Gert · Answer

The issue of centripetal jerk is apparent when considering the movement of the masses as the F is constant, implying a tangential acceleration. The equation for centripetal acceleration assumes a constant rotational velocity, which this does not have. Thus, we cannot use $a_c=omega r$ (where $omega$ is a constant), but its derivative, $j_c=alpha r$.

You really are starting from the wrong premise here.

The equation for centripetal acceleration does not assume a constant rotational velocity at all.

You're applying a constant torque $tau$:

$$tau=Fr$$

By Newton's second, here applied to rotation:

$$Ialpha=tau=Fr$$

Here $alpha=frac{domega}{dt}=dot{omega}$.

Since as:

$$alpha =frac{tau}{I}=frac{Fr}{I}$$

With $F=text{constant}implies alpha=text{constant}$.

Of course that means that $omega$ evolves with time:

$$dot{omega}=frac{Fr}{I}$$

$$implies int domega=intfrac{Fr}{I}dt=frac{Fr}{I}int dt$$

Integrate between suitable boundaries.

This problem involves no angular jerk.

Edit: in response to OP's comment.

If the masses $m$ are mobile then the inertial moment of one mass is (consider it a point mass):

$$I_m=m(L+Ssintheta)^2$$
From the free body diagram:
$$T=mgsintheta$$
$$F_c=m(L+Ssintheta)omega^2=Tsintheta=mgsin^2theta$$
$$(L+Ssintheta)omega^2=gsin^2theta$$
$$Lomega^2+Somega^2sintheta=gsin^2theta$$
Set:
$$x=sintheta$$
Then:

$$gx^2-Somega^2x-Lomega^2=0$$
$$Delta=S^2omega^4-4gLomega^2$$
$$x_{pm}=frac{Somega^2pmsqrt{Delta}}{2g}$$

$$theta=f(omega)$$
The total inertial moment then is:
$$I=I_T+2I_m=I_T+2m(L+Ssin f(omega))^2=I(omega)$$
$$dot{omega}=frac{Fr}{I(omega)}$$
The equation of motion becomes:
$$I(omega)domega=Frdt$$
Then $omega$ is no longer a linear function of $t$.

sammy gerbil · Answer

I think the problem (of finding how the moment of inertia of the apparatus varies with time) is far more difficult than you imagine. Also, as I said in my 1st comment, I think it is not worthwhile trying to solve it. It is a wild goose chase. It does not make much sense to try to measure something which changes as you measure it.

It would be difficult enough if this were a static problem, with constant angular velocity and constant moment of inertia. The balls would then make a constant angle $theta$ with the vertical, and they would be in the same plane as the cross-piece on the 'T'.

But this problem is a dynamic one. Angular velocity $omega$ is increasing, so the balls will swing upwards/outwards in the plane of the 'T' and also 'backwards' out of this plane, as I think you realise. The moment of inertia increases in a very complex manner.

Furthermore, the force $F=M(g-ddot y)$ is not constant because $ddot y=Rdot omega$ may change as moment of inertia increases. (Here $y$ is the vertical position of the falling mass, measured downwards.)

So the dynamical equation of motion will be very difficult to derive, and probably can only be solved by numerical analysis.

I think the simplest way in which you can get something out of the experiment is to remove the balls (or fix them in place so that they cannot move) and measure only the fixed moment of inertia of the 'T'. Call this $J_0$. The falling mass $M$ should then descend with uniform acceleration $ddot y$. This situation is far easier to analyse. If you plot a straight-line graph of $g/ddot y$ against $1/MR^2$ the slope is $J_0$.

Blacklight MG · Answer

This is a bit too late but I can answer this question. Even though there is an acceleration in the system, the radius is fixed so the centripetal acceleration will still be omega^2r. The velocity vector of circular motion is always tangential to the trajectory, so the change in speed should be due to an acceleration vector in the same direction. That means the total acceleration would be -omega^2r.(er) + dv/dt.(et), where (er) and (et) are unit vectors in the radially outward and tangential directions respectively (please pardon me for the notation, I'm typing this on my mobile, will change it when I get time). Because the total acceleration is a vector sum of tangential and radial vector, it will not be pointing towards the centre.
This is very nicely explained in Chapter 7 of the book "Concepts of Physics - Vol. 1" by HC Verma.
I'll still give a short derivation.
Consider two unit vectors (er) and (et) pointing radially outwards and tangential to a circle. By basic math, we get (er) = (i)cos(theta) + (j)sin(theta) and (et) = -(i)sin(theta) + (j)cos(theta).
Now consider a the radial vector (r) of the rotating body as (r) = r.(er).
Differentiating it w.r.t time,
(v) = d(r)/dt = d[r((i)cos(theta) + (j)sin(theta))]/dt
= r[(i).-sin(theta)d(theta)/dt + (j).cos(theta)d(theta)/dt]

= r.omega[-(i)sin(theta) + (j)cos(theta)]

= r.omega.(et)

Now again differentiating,
(a) = d(v)/dt = d[r.omega(-(i)sin(theta) + (j)cos(theta))]/dt
= r[omega.d(-(i)sin(theta) + (j)cos(theta))/dt + d(omega)/dt.(-(i)sin(theta) + (j)cos(theta))]

= omega.r[-(i)cos(theta)d(theta)/dt - (j)sin(theta)d(theta)/dt] + r.d(omega)/dt.(et)

= -omega^2.r((i)cos(theta) + (j)sin(theta)) + r(d(omega)/dt).(et)

= -omega^2.r.(er) + d(v)/dt.(et), because d(r.omega)/dt = dv/dt

Understanding a rotational system with centripetal snap, angular jerk, and a third-dimensional tension vector

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