Theoretical Reconstruction of Galileo’s Two-Bucket Experiment

Sylvio R. Bistafa

University of Sao Paulo, Sao Paulo, Brazil.

DOI: 10.4236/ahs.2018.73009                

Abstract

In the present work, the theoretical solution of a problem extracted from a historical context is addressed, in which Galileo supposedly conducted an experiment to measure the percussion force of a water jet. The experimental apparatus consists of a balance, in which a counterweight hangs on to one of its extremities, and two buckets hang on to the other extremity. The water jet from the bottom of the upper bucket strikes the lower bucket. The objective is to find the jet percussion force on the lower bucket. The result of the analysis revealed that the method proposed by Galileo for the calculation of the jet percussion force is incorrect. The analysis also revealed that the resultant force during the process is practically null, which would make Galileo’s account of the major movements of the balance credible, despite his having not identified all the forces acting on the system.

Keywords

Galilean Studies, History of Science, History of Scientific Instruments

1. Introduction

Galileo’s Discourses is originally divided into four days―as published in the Leiden edition of 1638―, to which were posthumously added another two days, all written in dialogic form in Two New Sciences. The Sixth Day was translated by Stillman Drake as the Added Day: On the Force of Percussion ( Drake, 1989 ), where the specific goal of the interlocutors Salviati, Sagredo and Aproíno is to understand and find a means of measuring the percussion force.

The first experiment about this force discussed by the trio begins when Aproíno narrates to Sagredo an experiment with two buckets conducted by the Academic (Galileo) to investigate the effect of the percussion force. In this experiment (see Figure 1), the upper bucket is filled with water and has a hole in the

Figure 1. A physical reproduction of Galileo’s two-bucket setup. This model is found at the University of Pavia, Italy ( Caffarelli , 2009: p. 9 ）

bottom. At the beginning of the experiment, the orifice is closed, and the balance is in equilibrium. Once the orifice is opened, the water flows to the lower bucket. Initially, the balance tilts to the counterweight side, and after the jet hits the lower bucket, the equilibrium is reestablished.

The present study has the objective of finding the forces acting on the balance in unsteady state, since the opening of the orifice in the bottom of the upper bucket until the end of the process, when all the water contained in this bucket has drained to the lower bucket. In the development of the theoretical model, we shall use the conservation equations of fluid mechanics in unsteady state, in the so-called integral form: continuity, in the form of conservation of the volume flux; energy, in the form provided by Torricelli’s law; and Newton’s 2nd law, best known in fluid mechanics as the linear momentum equation.

2. The Flow through the Orifice and the Formation of the Water Jet

The volume flux $Q_o=Q_o\left(t\right)$ through the orifice is given by (Ássy, 2004)

$Q_o=C_d{S}_o\sqrt{2g{h}_s},$ (1)

in which $C_d$ is the discharge coefficient, $S_o$ is the area of the orifice, $h_s=h_s\left(t\right)$ is the water height from the orifice up to the free surface of the water in the upper bucket at instant t, and g is the gravity. Since Torricelli’s law says $V_o=\sqrt{2g{h}_s}$ , then we can write Equation (1) as $Q_o=C_d{S}_o{V}_o$ .

The discharge coefficient $C_d$ consists of the product of two other coefficients, namely: the contraction coefficient $C_c$ , and the velocity coefficient $C_v$ , such that $C_d=C_c{C}_v$ .

The origin of the contraction coefficient $C_c$ is due to the fact that, as experience shows, the liquid jet cross section at the plane of the orifice $S_o$ continues to contract, until reaching a minimum section, which occurs at a small distance from $S_o$ , called vena contracta, which is crossed by trajectories that are sensible

straight and parallel, in which the velocity is uniform, and the pressure is atmospheric, with the contraction coefficient theoretically given by $C_c=\frac{\text{π}}{\text{π}+2}\approx 0.611$ .

Torricelli’s law refers to the velocity at the vena contracta: in the plane of the orifice, neither the pressure, nor the velocity is uniform, and the velocity is lower than the velocity at the vena contracta.

The velocity given by Torricelli’s law $V_o=\sqrt{2g{h}_s}$ is, however, a theoretical velocity that does not consider the fluid internal viscous forces. Thus, the actual velocity ${V^{\prime }}_o$ can be obtained by correcting the theoretical velocity $V_o$ with the velocity coefficient $C_v$ , whose value is experimentally obtained. In this way, the actual velocity at the vena contracta is ${V^{\prime }}_o$ , and given by ${V^{\prime }}_o=C_v{V}_o=C_v\sqrt{2g{h}_s}$ . From this, appears the expression for the volume flux through the orifice as $Q_o=C_c{C}_v{S}_o\sqrt{2g{h}_s}=C_d{S}_o\sqrt{2g{h}_s}$ , where $C_d=C_c{C}_v$ .

Experience also shows that the cross section of the falling water jet continues to contract, assuming a tapered form as shown in Figure 2. The shape of the jet during descent may be obtained by applying Bernoulli’s equation between point A, at elevation $z_A$ , and point B, at elevation $z_B$ , in the form

Figure 2. A fluid jet extruded from an orifice accelerates under the influence of gravity. Its shape is influenced both by the gravitational acceleration and surface tension.

$\frac{1}{2}\rho {V^{\prime }}_o^2+\rho g{z}_A+p_A=\frac{1}{2}\rho V^2\left(z\right)+\rho g{z}_B+p_B$ , (2)

where ${V^{\prime }}_o$ is the velocity at the vena contracta, whose cross section has a radius a, $V\left(z\right)$ is the velocity at the section whose radius is r(z), ρ is the density, and $p_A$ and $p_B$ are the absolute pressures at A and B, respectively.

The average local curvature k of slender threads may be approximately expressed as $k\approx \frac{1}{r\left(z\right)}$ . Therefore, the pressures at points A and B may be simply related to the ambient pressure $p_{atm}$ by: $p_A\approx p_{atm}+\frac{\sigma }{a}$ , $p_B\approx p_{atm}+\frac{\sigma }{r\left(z\right)}$ , where $\sigma$ is the surface tension. Substituting these results into Equation (2), we have

$\frac{1}{2}\rho {V^{\prime }}_o^2+\rho g{z}_A+p_{atm}+\frac{\sigma }{a}=\frac{1}{2}\rho V^2\left(z\right)+\rho g{z}_B+p_{atm}+\frac{\sigma }{r\left(z\right)}$ , (3)

Disregarding the surface tension effects on the shape of the jet, then Equation (3) may be rewritten as

$\frac{V\left(z\right)}{{V^{\prime }}_o}={\left[1+\frac{2g\left(z_A-z_B\right)}{{V^{\prime }}_o^2}\right]}^{1/2}$ . (4)

When applying the continuity equation in terms of conservation of the volume flux, for which $\text{π}{a}^2{V^{\prime }}_o=\text{π}{r}^{2}V\left(z\right)$ , it is possible to rewrite Equation (4) in the form

$\frac{r^2}{a^2}={\left[1+\frac{2g\left(z_A-z_B\right)}{{V^{\prime }}_o^2}\right]}^{-1/2}$ . (5)

Since $C_c{S}_o=\text{π}{a}^2$ , then the area S of any flow cross section is readily obtained from Equation (5) as

$S=C_c{S}_o{\left[1+\frac{2g\left(z_A-z_B\right)}{{V^{\prime }}_o^2}\right]}^{-1/2}=C_c{S}_o{\left(1+\frac{H}{C_v^2{h}_s}\right)}^{-1/2}$ , (6)

where $H=H\left(t\right)=z_A-z_B$ is the jet height at instant t.

The jet volume ${\sout{V}}_j\left(t\right)$ , at instant t, will be given by

$\begin{array}{c}{\sout{V}}_j\left(t\right)={\displaystyle {\int }_0^{H}S\text{d}h}=C_c{S}_o{\displaystyle {\int }_0^H{\left(1+\frac{h}{C_v^2{h}_s}\right)}^{-1/2}\text{d}h}\\ =2S_o{C}_v^2{C}_c{h}_s\left(t\right)\left[{\left(1+\frac{H\left(t\right)}{C_v^2{h}_s\left(t\right)}\right)}^{1/2}-1\right].\end{array}$ (7)

3. Theoretical Model for the Two-Bucket Experiment in Unsteady State

We present next the linear momentum equation, in the form applicable to the unsteady flow in a control volume Ω, limited by the water contained in the bucket at each instant, as (Ássy, 2004)

$G+R=\frac{\partial }{\partial t}{\displaystyle \underset{\Omega }{\int }\rho v\text{d}\Omega }+Q_m{V}_e{n}_e+Q_m{V}_s{n}_s$ , (8)

where $G$ is the resultant of the applied body forces (e.g. fluid weight), $R$ is the resultant of the forces of contact that act at the walls of control volume; $\frac{\partial }{\partial t}{\displaystyle \underset{\Omega }{\int }\rho v\text{d}\Omega }$ is the momentum variation inside the control volume Ω; $v$ is the

fluid velocity, $Q_m{V}_e{n}_e$ and $Q_m{V}_s{n}_s$ are the momentum fluxes at the inlet and at the outlet of the control volume, respectively. $Q_m$ is the mass flux, $V_e$ and $V_s$ are the velocities at the inlet and outlet cross sections of the control volume, respectively, and $n_e$ and $n_s$ are the unit normal vectors at these flow cross sections. The mass flux $Q_m$ can be written as $Q_m=\rho Q$ , where Q is the volume flux and $\rho$ is the density of the water (mass per unit of volume).

3.1. Resultant Force on the Upper Bucket in Unsteady State

The integral $\frac{\partial }{\partial t}{\displaystyle \underset{\Omega }{\int }\rho v\text{d}\Omega }$ in Equation (8) is the time variation of momentum

inside the control volume, which corresponds to a vertical force that decelerates the water mass contained in the upper bucket in its descending motion. During the drainage of the upper bucket, this force acts upward, according to $e_z$ (the upward unit vector), decelerating the mass of water in its descending motion. Since, by hypothesis, all the water particles inside Ω move downward with the

same velocity of the free surface $V_e$ , then, the integral $\frac{\partial }{\partial t}{\displaystyle \underset{\Omega }{\int }\rho v\text{d}\Omega }=\rho {\displaystyle \underset{0}{\overset{h_s}{\int }}\frac{\partial V_e}{\partial t}{S}_e\text{d}h}$ , in which $S_e$ is the area of the flow cross sections in the upper bucket.

The integral $\rho {\displaystyle \underset{0}{\overset{h_s}{\int }}\frac{\partial V_e}{\partial t}{S}_e\text{d}h}=\rho S_e{h}_s\frac{\partial V_e}{\partial t}$ , in which $h_s=h_s\left(t\right)$ is the height of the free surface of the water in upper bucket at instant t. In this expression, $\frac{\partial V_e}{\partial t}$ is the acceleration to which the water in the upper bucket is subjected to during its descending motion. Then, $\frac{\partial V_e}{\partial t}=\frac{\partial V_e}{\partial t}\left(-e_z\right)$ , and, since $V_e=C_d\frac{S_o}{S_e}\sqrt{2g{h}_s}$ , results in $\frac{\partial V_e}{\partial t}=C_d\frac{S_o}{S_e}\frac{g}{\sqrt{2g{h}_s}}\frac{\partial h_s}{\partial t}\left(-e_z\right)$ .

But, from continuity $\frac{\partial h_s}{\partial t}=-C_d\frac{S_o}{S_e}\sqrt{2g{h}_s}$ , and then, $\frac{\partial V_e}{\partial t}=g{C}_d^2{S}_e{\left(\frac{S_o}{S_e}\right)}^2{h}_s\left(e_z\right)$ . Then, finally, $\frac{\partial }{\partial t}{\displaystyle \underset{\Omega }{\int }\rho v\text{d}\Omega }$ can be written as

$\frac{\partial }{\partial t}{\displaystyle \underset{\Omega }{\int }\rho v\text{d}\Omega }=\rho g{C}_d^2{S}_e{\left(\frac{S_o}{S_e}\right)}^2{h}_s\left(e_z\right),$ , (9)

for the upper bucket.

Substituting Equation (9) into Equation (8), and considering that in Equation

(8) the momentum flux $Q_m{V}_e{n}_e=2\rho g{C}_d^2\frac{S_0^2}{S_e}{h}_s\left(e_z\right)$ and the momentum flux $Q_m{V}_s{n}_s=2\rho g{C}_d{C}_v{S}_o{h}_s\left(-e_z\right)$ , results in

$\begin{array}{l}{R}_{bs}=G_{lbs}\left(e_z\right)+\rho g{C}_d^2{S}_e{\left(\frac{S_o}{S_e}\right)}^2{h}_s\left(e_z\right)\\ +2\rho g{C}_d^2\frac{S_0^2}{S_e}{h}_s\left(e_z\right)+2\rho g{C}_d{C}_v{S}_o{h}_s\left(-e_z\right),\end{array}$ , (10)

in which $G_{lbs}$ is the weight of the water contained in the upper bucket. $R_{bs}$ , as given by Equation (10), is the resultant force acting on the water body contained in the upper bucket in unsteady state.

3.2. Resultant Force on the Lower Bucket in Unsteady State

As far as the lower bucket is concerned, the velocity of the jet as it strikes the bottom of this bucket changes its direction from axial to the radial direction; then,

$V_e=V_e\left(-e_z\right)=0$ .Therefore, for the lower bucket $\frac{\partial }{\partial t}{\displaystyle \underset{\Omega }{\int }\rho v\text{d}\Omega }=\rho {\displaystyle \underset{\Omega }{\int }\frac{\partial V_e}{\partial t}\text{d}\Omega }=0$ .

The momentum flux of the jet falling on the free surface of the lower bucket is given by $Q_m{V}_e{n}_e=\rho Q{V}_e\left(e_z\right)$ , where $Q=Q\left(t\right)$ is the volume flux that enters the lower bucket, and that varies with the time in the unsteady state.

For a fixed control volume that incorporates the volume of the water jet, the continuity equation, in unsteady state, for an incompressible fluid may be written as

$Q=Q_o-\frac{\partial }{\partial t}{\displaystyle \underset{{\sout{V}}_j}{\int }\text{d}{\sout{V}}_j}=Q_o-\frac{\partial V_j}{\partial t}$ , (11)

in which $Q_o=C_d{S}_o\sqrt{2g{h}_s}$ is the volume flux through the orifice and ${\sout{V}}_j$ is the volume of the jet at each instant, as given by Equation (7).

Applying Equation (7) in the assessment of $\frac{\partial {\sout{V}}_j}{\partial t}$ we have that

$\frac{\partial V_j}{\partial t}=\frac{\partial }{\partial t}\left\{2S_o{C}_v^2{C}_c{h}_s\left[{\left(1+\frac{H}{C_v^2{h}_s}\right)}^{1/2}-1\right]\right\}$ . (12)

Once the derivative indicated in Equation (12) has been evaluated, and substituting the resulting expression into Equation (11), gives

$Q=Q_o\left\{1-2\frac{S_o}{S_e}{C}_v^2{C}_c\left[\frac{1}{2C_v^2}\left(\frac{H}{h_s}-1\right){\left(1+\frac{H}{C_v^2{h}_s}\right)}^{-1/2}-{\left(1+\frac{H}{C_v^2{h}_s}\right)}^{1/2}+1\right]\right\}$ . (13)

Then, the momentum flux of the jet that falls on the free surface of the lower bucket $Q_m{V}_e{n}_e=\rho Q{V}_e\left(e_z\right)$ , with $V_e=\frac{Q}{S}$ ,in which S is the area of the jet cross section when falling on the free surface. This area is given by Equation (6), repeated here as $S=C_c{S}_o{\left(1+\frac{H}{C_v^2{h}_s}\right)}^{-1/2}$ ; and, therefore, $Q_m{V}_e{n}_e=\rho \frac{Q^2}{S}\left(e_z\right)=\rho Q^2{\left(C_c{S}_o\right)}^{-1}{\left(1+\frac{H}{C_v^2{h}_s}\right)}^{1/2}\left(e_z\right)$ .

On the other hand, the momentum flux at the lower bucket free surface will be given by $Q_m{V}_s{n}_s=\rho \frac{1}{S_e}{Q}^2\left(e_z\right)$ , where $S_e$ is the free surface area of the lower bucket.

Then, from these results, we may write Equation (8) for the lower bucket as

$R_{bi}=G_{lbi}\left(e_z\right)+\rho Q^2{\left(C_c{S}_o\right)}^{-1}{\left(1+\frac{H}{C_v^2{h}_s}\right)}^{1/2}\left(e_z\right)+\rho \frac{1}{S_e}{Q}^2\left(e_z\right)$ , (14)

in which $G_{lbi}$ is the weight of the water contained in the lower bucket, with Q given by Equation (13). $R_{bi}$ , as given by Equation (14), is the resultant force acting on the water body contained in the lower bucket in unsteady state.

3.3. Resultant Force on the Balance in Unsteady State

The resultant force on the balance $R_b$ will be given by the sum of − $-R_{bs}$ (Equation 10) and − $-R_{bi}$ (Equation 14). By considering that the weight of the water in the system $G_l$ may be written as $G_l=G_j\left(t\right)+G_{lbs}\left(t\right)+G_{lbi}\left(t\right)$ , or $G_l-G_j\left(t\right)=G_{lbs}\left(t\right)+G_{lbi}\left(t\right)$ , where $G_j(t)=\rho g{\sout{V}}_j\left(t\right)$ is the weight of the water jet suspended in the air between the two buckets at instant t, the resultant force on the balance will be given by

$\begin{array}{c}{R}_b=\{G_l-G_j\left(t\right)+\rho g{C}_d^2{S}_e{\left(\frac{S_o}{S_e}\right)}^2{h}_s+2\rho g{C}_d^2\frac{S_0^2}{S_e}{h}_s-2\rho g{C}_d{C}_v{S}_o{h}_s\\ +\rho Q^2{\left(C_c{S}_o\right)}^{-1}{\left(1+\frac{H}{C_v^2{h}_s}\right)}^{1/2}+\rho \frac{1}{S_e}{Q}^2\}\left(-e_z\right).\end{array}$ (15)

The division of Equation (15) by the weight of the water contained in the system $G_l$ , and given by $G_l=\rho gL{S}_e$ , where L is the height of the water in the upper bucket at the beginning of its drainage, gives the dimensionless form of this equation as

$\begin{array}{c}\frac{R_b}{G_l}=\{\frac{G_l}{\rho gL{S}_e}-2C_d{C}_{v}R{C}^{-1}{H}_s\left[{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}-1\right]+C_d^{2}R{C}^{-2}{H}_s+2C_d^{2}R{C}^{-2}{H}_s\\ -2C_d{C}_{v}R{C}^{-1}{H}_s+\frac{Q^2}{gL{S}_e}{\left(C_c{S}_o\right)}^{-1}{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}+\frac{Q^2}{gL{S}_e^2}\}\left(-e_z\right).\end{array}$ . (16)

Calling $\frac{h_s}{L}$ by $H_s$ , $\frac{H}{L}$ by $H$ , and $\frac{S_e}{S_o}$ by RC, where RC is the contraction ratio, then Equation (16) may be rewritten in the most general form as

$\begin{array}{c}\frac{R_b}{G_l}=\{\frac{G_l}{\rho gL{S}_e}-2C_d{C}_{v}R{C}^{-1}{H}_s\left[{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}-1\right]+C_d^{2}R{C}^{-2}{H}_s+2C_d^{2}R{C}^{-2}{H}_s\\ -2C_d{C}_{v}R{C}^{-1}{H}_s+\frac{Q^2}{gL{S}_e}{\left(C_c{S}_o\right)}^{-1}{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}+\frac{Q^2}{gL{S}_e^2}\}\left(-e_z\right).\end{array}$ . (17)

Let us rename the terms that appear in Equation (17), by calling: $A=\frac{G_l}{\rho gL{S}_e}=1$ , the relative weight of the water contained in the system; $B=2C_d{C}_{v}R{C}^{-1}{H}_s\left[{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}-1\right]$ , the relative weight of the water suspended in the air between the orifice and the free surface of the lower bucket; $C=C_d^{2}R{C}^{-2}{H}_s$ , the relative variation of momentum in the upper bucket; $D=2C_d^{2}R{C}^{-2}{H}_s$ , the relative momentum flux at the upper bucket free surface; $E=2C_d^2{C}_c^{-1}R{C}^{-1}{H}_s$ , the relative momentum flux at the orifice; $F=\frac{Q^2}{gL{S}_e}{\left(C_c{S}_o\right)}^{-1}{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}$ , the relative momentum flux of the jet that falls into the free surface of the lower bucket; and $G=\frac{Q^2}{gL{S}_e^2}$ , the relative momentum flux at the free surface of the lower bucket.

By substituting Q, given by Equation (13), into the expressions for F and G, the result is

$\begin{array}{c}F=2C_d^3{C}_c^{-1}R{C}^{-1}{H}_s\{1-2C_v^2{C}_{c}R{C}^{-1}[\frac{1}{2C_v^2}\left(\frac{H}{H_s}-1\right){\left(1+\frac{H}{C_v^2{H}_s}\right)}^{-1/2}\\ -{{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}+1]\}}^2{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}.\end{array}$ . (18)

$\begin{array}{c}G=2C_d^{2}R{C}^{-2}{H}_s\{1-2C_v^2{C}_{c}R{C}^{-1}[\frac{1}{2C_v^2}\left(\frac{H}{H_s}-1\right){\left(1+\frac{H}{C_v^2{H}_s}\right)}^{-1/2}\\ -{{\left(1+\frac{H}{C_v^2{H}_s}\right)}^{1/2}+1]\}}^2.\end{array}$ . (19)

Finally, we may write Equation (17) in a more compact form, as

$\frac{R_b}{\rho gL{S}_e}=\left(A-B+C+D-E+F+G\right)\left(-e_z\right).$ . (20)

Figure 3 highlights the forces that appear in Equation (20).

To numerically evaluate Equation (20), we need, now, an expression that relates the time elapsed to the height of the water free surface in the upper bucket. For the determination of this elapsed time, we shall write the continuity equation for the

upper bucket in the form $Q\left(t\right)=-S_e\frac{\text{d}{h}_s}{\text{d}t}$ , where $Q\left(t\right)=C_d{S}_o\sqrt{2g{h}_s}$ ; and hence

$\frac{\text{d}{h}_s}{\text{d}t}=-C_d\frac{S_o}{S_e}\sqrt{2g{h}_s}.$ (21)

Upon integration, Equation (21) yields

$t=\frac{S_e}{C_d{S}_o}\sqrt{\frac{2}{g}}\left(\sqrt{h_o}-\sqrt{h_s}\right),$ (22)

Figure 3. Relative forces acting on the balance: weight of the water in the system―A, weight of the jet―B, variation of momentum in the upper bucket―C, momentum flux at free surface of the upper bucket―D, reaction force on the upper bucket―E, percussion force on the lower bucket―F, momentum flux at the free surface of the lower bucket―G.

where $h_o=h\left(t=0\right)=L$ .

By writing $\frac{S_e}{S_o}=RC$ , $\frac{h_0}{L}=1$ , and $\frac{h_s}{L}=H_s$ , then Equation (22) is transformed into

$t=\frac{RC}{C_d}\sqrt{2\frac{L}{g}}\left(1-\sqrt{H_s}\right),$ (23)

valid for $0\le H_s\le 1$ . This expression will give the time elapsed since the opening of the orifice, until the instant when the water height in the upper bucket reaches the value $H_s$ .

Galileo, supposedly used in his experiment elements with the following dimensions (Drake, 1989): distance between the bottoms of the buckets $H_i$ equal to 1.35 m (two braccia; one braccio ~ 67 cm), and orifice with diameter1 equal to 0.03 m. The diameter of the buckets and the water height in the upper bucket L are not narrated, and, therefore, it was assumed that both are equal to 0.3 m. For these dimensions, the volume of water contained in the system is 21.2 liters, with a mass of 21.2 kg and a weight of 208 N, approximately. This is the weight of the water contained in the system, called here as $G_l$ . With these numerical values,

we have $RC=\frac{S_e}{S_o}={\left(\frac{0.3\text{m}}{0.03\text{m}}\right)}^2=100$ .

The following values for the flow coefficients were adopted in the calculations as representative of the process: $C_c=0.63$ , $C_v=0.97$ , $C_d=0.61$ (Ássy, 2004).

Figure 4 presents the forces acting on the balance, obtained using Equation (20) and (23), for $RC=100$ , since the opening of the orifice in the bottom of the upper bucket, until its complete drainage. In this figure, forces with positive values tend to move the balance toward the buckets’ side, whereas forces with negative values tend to move the balance toward the counterweight side.

It is clearly seen in Figure 4 that the forces that dominate the process are: the weight of the jet―B, the reaction force on the upper bucket―E, and the percussion force on the lower bucket―F. The force generated by the momentum variation in the upper bucket―C, the force generated by the momentum flux at the free surface of the upper bucket―D, and the force generated by the momentum flux at the free surface of the lower bucket―G are practically null during the entire drainage process. Figure 4 also indicates that, after the first percussion of

Figure 4. Forces acting on the balance, since the opening of the orifice in the upper bucket, until the lower bucket is completely filled, for RC = 100. Weight of the jet―B, variation of momentum in the upper bucket―C, momentum flux at free surface of the upper bucket―D, reaction force on the upper bucket―E, percussion force on the lower bucket―F, momentum flux at the free surface of the lower bucket―G, and the Resultant Force.

the jet in the lower bucket, the resultant force is practically null during the upper bucket drainage. Thus, accordingly, the balance, that was inclined toward the counterweight side after the opening of the orifice, will tend to return to the equilibrium position, remaining, however, still a little inclined toward the buckets side during the process.

4. Discussion

For Galileo, the percussion force would be equal to the weight of the jet that is suspended in the air between the waters in the two buckets (Drake, 1989). However, Figure 5 shows that the percussion force has a different behavior from the weight of the jet, with a value always greater during the upper bucket drainage.

Aproíno, in his talk (Drake, 1989), states that the weight of the jet would be “certainly” 10 to 12 pounds, although Salviati indicates in his replica that there would be some uncertainty due to the “difficulty in measuring the amount of the falling water”. Although Aproíno does not mention at which instant of time this value would have been obtained, it may be admitted that it could be at the instant when the jet first strikes the lower bucket. At this instant, the percussion force corresponds to, approximately, 2.8% of the weight of water contained in the system, which gives 1.75 pounds.² At this same instant of time, the weight of

Figure 5. Moduli of the forces acting on the balance, for RC = 100.

the jet corresponds, approximately, to 1.7% of the weight of water contained in the system, that is, 1.06 pounds, which is a much lower value than that estimated by Galileo.

Figure 5 also indicates that during the drainage of the upper bucket, the percussion force is practically equal to the sum of the weight of the jet, plus the reaction force in the upper bucket. The small difference between the percussion force and this sum is practically constant during the entire process, around 0.03% of the weight of the water contained in the system, corresponding to a resultant of only 0.062 N (6.4 grams), approximately, in favor of the percussion force. This resultant will cause the balance to remain a little unbalanced toward the buckets side during the upper bucket drainage.

5. Conclusion

The analysis made demonstrates that the percussion force on the lower bucket does not correspond to the weight of the jet that is suspended in the air between the waters in the two buckets, upper and lower, as suggested by Galileo. In fact, the percussion force is proportional to the square of the jet velocity, assuming a value always greater than the weight of the jet during the upper bucket drainage.

During the upper bucket drainage, the balance will remain a little unbalanced toward the side of the buckets, but due to the small magnitude of the resultant force, with a value practically constant, and around 6.4 grams only during the entire process―which would make the unbalance of the balance described by Galileo small enough to pass unnoticed―, indicates that the report of Galileo could be considered as being credible “[…] but the water had hardly begun to strike against the bottom of the lower bucket when the counterweight ceased to descend, and commenced to rise with very tranquil motion, restoring itself to equilibrium while water was still flowing, and upon reaching equilibrium it balanced and came to rest without passing a hairbreadth beyond” (Drake, 1989).

Conflicts of Interest

The authors declare no conflicts of interest regarding the publication of this paper.

NOTES

¹Galileo indicates that “[…] The bottom of the upper bucket had been pierced by a hole the size of an egg or a little smaller” (Drake, 1989). There is no doubt that nowadays, the eggs are greater than their homologues in Galileo’s time. A search over the Internet revealed that the average diameter of a chicken egg in its larger cross section is around 4.25 cm. A diameter of this magnitude would drain the bucket very quickly, not allowing an adequate observation of the movement of the balance. For these reasons, it was decided to adopt an orifice diameter of 3 cm.

²1 Tuscan pound = 0.3395 kg (Caffarelli, 2009).

Conflicts of Interest

The authors declare no conflicts of interest.

References

[1]	Assy, T. M. (2004). Mecanica dos Fluidos: Fundamentos e Aplicacoes (2nd Ed.). (Rio de Janeiro: LTC.
[2]	Caffarelli, R. V. (2009). Galileo Galilei and Motion—A Reconstruction of 50 Years of Experiments and Discoveries (Jointly Published by Springer & Società Italiana di Fisica).
[3]	Drake, S. (1989). Galileo Galilei: Two New Sciences (2nd Ed., pp. 281-342). Ontario: Wall & Emerson, Inc. http://www.spirasolaris.ca/sbb6Added_Day.pdf