Kvant

Rough automatic draft, low quality: expect mistakes and awkward wording. It will be replaced by a better translation. Original →

26

LABORATORY “QUANTA”
with EXPERIENCES
PENDULUM
G.L.Kotkin

It is difficult to find physical devices that were as simple in design and reliable in use as matnikki. Meanwhile, experiments with them can lead to interesting results, which are extremely important not only in mechanics, but also in radio engineering and electrical engineering. Try to do the suggested experiments yourself and explain the effects that you will observe. Although the experiments themselves are very simple, however, it is not easy to fully understand the increase in matniki: for this you need to know the basic laws of harmonic vibrations and have experience in trigonometric transformations. Apparently, only tenth graders will be able to fully understand this article, but schoolchildren in grades 8-9 can carry out these experiments and fully explain them, at least qualitatively.

Matnik with suspension division

Make a mat with a split hanger, shown at figure 1. The length of the mat ll should be much longer than the length of the top divided part of the hanger.

Push the mat at an angle to the figure plane. You will see that at first the matnik will be qualitatively in the direction only, but soon its movement will turn into rotation in the circle of the vertical axis. Then the mat will begin to oscillate again in the plane, but no longer in the one in which it was pushed. After this, the rotation will begin again, but in the other direction. Gradually it will be replaced by movement in the direction of the first oscillatory shock. Then everything will repeat again from the beginning.

What is the reason for this behavior of the matnik?

Related matniki

a) Two identical mats (for example, nuts on a thread) will be hung on a not very tight stretched thread ABAB (Fig. 2). Reject one of the matniks and release.

Fig. 1. Fig. 2.

27

Try changing the weights of the weights, changing the lengths of the threads of the mats, and the tension of the upper thread.

  1. Attach two matrices to the rigid frame. Then tie the threads of the matniks with a thread at a certain height (Fig. 3). Reject one of the mats and lower it. Look how the matniki will move.

Double matnik

The structure of the double matnik is shown in figure 4. The upper weight is much heavier than the lower one, and the long threads are the same. Push the bottom weight and watch it move.

Let’s now understand the behavior of these matniks.

  1. Let’s start with a matnik with an unlinked suspension.

The rather complex behavior of the matnik that you observe can be explained by the fact that its movement consists of two oscillatory movements (Fig. 5): parallel to the plane zyzy and perpendicular to it. These oscillations occur independently of each other (if the deviations of the mat from the vertical are not too large), and the periods of their corresponding ones are equal

T1=2πlgT2=2πLg.T_1 = 2\pi \sqrt{\frac{l}{g}} \quad T_2 = 2\pi \sqrt{\frac{L}{g}}.

First of all, let’s learn how to describe the movement of a weight using coordinates.

Let the point AA move along a circle of radius aa with an angular velocity ω\omega counterclockwise (Fig. 6a) or clockwise (Fig. 66). Then the projection BB of the point AA onto the axis xx performs a harmonic oscillation*) with an angular frequency ω\omega equal to 2πT\frac{2\pi}{T} and an amplitude aa.

The projection CC of the same point AA onto the axis yy makes similar oscillations, but reaches its maximum deviation from point OO a quarter of a period later - after the time during which the radius OAOA makes 14\frac{1}{4} revolutions around the point OO. It is easy to verify this by following the movements of points CC and BB when rotating the radius OAOA. At the moment when the projection of the point AA onto the axis xx is maximally deviated from the point OO, its projection onto the axis yy is just

*) See, for example, the article by Ya. A. Smorodinsky “Similar movements”, «Kvant» No. 9, 1971.

29

direction ODOD (Fig. 7) to a distance aa and then release, then the coordinates of the weight will change according to the formulas:

{x=acos⁡ω1t,y=acos⁡ω2t,\begin{cases} x = a \cos \omega_1 t, \\ y = a \cos \omega_2 t, \end{cases}

Where

ω1=2πT1=gl,\omega_1 = \frac{2\pi}{T_1} = \sqrt{\frac{g}{l}},

ω2=2πT2=gL,\omega_2 = \frac{2\pi}{T_2} = \sqrt{\frac{g}{L}},

a=b2.a = \frac{b}{\sqrt{2}}.

Recall that ll and LL have very little difference from each other, that is, the frequencies of ω1\omega_1 and ω2\omega_2 are almost the same. Therefore, at first, oscillations along the xx and yy axis will occur almost in phase.

Since ω1>ω2\omega_1 > \omega_2, over time the oscillation along the yy axis lags behind the oscillation along the xx axis more and more. But, as we have seen, when a point moves counterclockwise around a circle, the oscillations of its projections on the xx and yy axes lag behind each other by the fourth period. It follows that when the lag of the oscillations of the weight along the axes xx and yy reaches the fourth period, it will move just along the circle counterclockwise. When the oscillations of the weight lag along the axes xx and yy on the field of motion, it will move along the straight line E′D′E'D'. Then the lag of the oscillation along the yy axis will reach the 34\frac{3}{4} period - the weight moves around the circle clockwise. Finally, when there is a delay of an entire period, the weight again oscillates along the straight line EDED. This is what you observed.

It is convenient to “retell” these wonders using formulas. System (5) can be represented as

{x=acos⁡ω1t,y=acos⁡(ω1t−ϕ),\begin{cases} x = a \cos \omega_1 t, \\ y = a \cos (\omega_1 t - \phi), \end{cases}

where ϕ=(ω1−ω2)t\phi = (\omega_1 - \omega_2) t. Over two or three periods, ϕ\phi remains almost unchanged, but over many periods it increases steadily. For ϕ=0,π2,π,3π2\phi = 0, \frac{\pi}{2}, \pi, \frac{3\pi}{2}, formulas (6) coincide in sequence with formulas (3), (1), (4), (2).

Fig. 9.

At ϕ=2π\phi = 2\pi the weight returns to motion in a straight line EDED.

The stated theory can be tested experimentally. After all, we can calculate how long it will take for the weight to move through the entire cycle of changes. If it is time T0T_0, then ϕ0=(ω1−ω2)T0=2π\phi_0 = (\omega_1 - \omega_2) T_0 = 2\pi, opening 2πT0=ω1−ω2\frac{2\pi}{T_0} = \omega_1 - \omega_2, or

1T0=1T1−1T2.\frac{1}{T_0} = \frac{1}{T_1} - \frac{1}{T_2}.

Now you need to measure the oscillation periods T1T_1 and T2T_2 of the pendulum, then in the yzyz plane, another time in the xzxz plane. Time T0T_0 is measured independently. After measuring T1T_1, T2T_2 and T0T_0, check the correctness of formula (7). To measure T1T_1 and T2T_2 it is better to determine the time, say, in 10-15 vibrations. It is immediately revealed what reasons lead to deviations from the calculation. Apparently, the damping of oscillations caused by air resistance is primarily affected. Well, the weights shouldn’t be too light.

In reality, the movements will not occur in a straight line or circle, but along a complex trajectory. This trajectory (Fig. 9) more or less uniformly “fills” the entire square.

If the initial angle with the symmetry plane is different from π4\frac{\pi}{4}, then the characteristic “instantaneous” trajectories of the weight are the diagonals of the right angle and the ellipses inscribed in it.

The fact that the movement of the pendulum consists of independent oscillations is expressed by saying that the superposition principle is valid for its oscillations *).

  1. Let’s move on to explaining the movement of the connected pendants (Fig. 2 and 3). If we deflect and then release one of them, we will see that the other will gradually begin to move.

*) Reader «Kvant» have already encountered the principle of superposition when explaining the type of wave on the surface of water («Kvant» No. 1, 1971, p. 32).

30

This is explained by the fact that when the first matrix is ​​deflected by the bond, their thread is deformed and the elastic force acts on the other matrix, imparting acceleration to it. The first matrix will oscillate with less and less amplitude and finally stop. At this time, the amplitude of vibrations of the second matrix will be the most magnificent. Then the first matrix will roll out, and the second will stop, and so on.

The complex oscillatory motion of a system consisting of two matrices can be represented as the result of the addition (superposition) of two oscillations with frequencies ω1\omega_1 and ω2\omega_2. One of the frequencies is equal to the frequency with which both matrices will oscillate if they are simultaneously deflected in one direction and then released (Fig. 10). Let’s denote this frequency by ω1\omega_1. Another frequency is ω2\omega_2. This is the frequency with which both matrices will vibrate if they are first simultaneously deflected in opposite directions and then released (Fig. 11).

Note that the angular frequency ω2\omega_2 is greater than the angular frequency ω1\omega_1. These two vibrations are called normal vibrations of two coupled matrices.

Let’s write the equation of normal vibrations. First

{x1′=acos⁡ω1t,x2′=−acos⁡ω1t,\begin{cases} x_1' = a \cos \omega_1 t, \\ x_2' = -a \cos \omega_1 t, \end{cases}

second

{x1′′=acos⁡ω2t,x2′′=acos⁡ω2t.\begin{cases} x_1'' = a \cos \omega_2 t, \\ x_2'' = a \cos \omega_2 t. \end{cases}

Let’s add the mixtures x1′x_1' with x1′′x_1'' and x2′x_2' with x2′′x_2''. We get:

{x1=x1′+x1′′=acos⁡ω1t+acos⁡ω2t,x2=x2′+x2′′=−acos⁡ω1t+acos⁡ω2t.\begin{cases} x_1 = x_1' + x_1'' = a \cos \omega_1 t + a \cos \omega_2 t, \\ x_2 = x_2' + x_2'' = -a \cos \omega_1 t + a \cos \omega_2 t. \end{cases}

Using the formula for adding cosines, we get:

{x1=Acos⁡Ωt,Ω=ω1+ω22,A=2acos⁡(ω1−ω22t).\begin{cases} x_1 = A \cos \Omega t, \quad \Omega = \frac{\omega_1 + \omega_2}{2}, \\ A = 2a \cos \left( \frac{\omega_1 - \omega_2}{2} t \right). \end{cases}

Due to the fact that ω1\omega_1 differs little from ω2\omega_2, the expression cos⁡(ω1−ω22t)\cos \left( \frac{\omega_1 - \omega_2}{2} t \right) is close to 1 (if ω1\omega_1 is equal to ω2\omega_2, then this expression is equal to 1). Therefore, it has little effect on the value of x1x_1. Therefore, the factor 2acos⁡(ω1−ω22t)2a \cos \left( \frac{\omega_1 - \omega_2}{2} t \right) in the expression for x1x_1 can be considered as slowly changing the amplitude (red point on Fig. 12, a). The situation is similar