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In this chapter, we will switch to using energy to solve physical problems instead of Newton’s laws and momentum. We will review the concepts of work, kinetic energy, and potential energy, and we will introduce conservative forces.

8.1 Introduction to Work and Energy

When a force is applied to an object such that it moves a displacement of Δr\Delta \vec{r}, work is done by that force. Work is defined as:

W=FdrW = \int \vec{F} \cdot \mathrm{d}\vec{r}

where F\vec{F} is the force and dr\mathrm{d}\vec{r} represents a small displacement.

If the force is constant, then you can simplify the above equations to:

W=Fdr=FΔr=FxΔx+FyΔy+FzΔzW = \vec{F} \cdot \int \mathrm{d}\vec{r} = \vec{F} \cdot \Delta \vec{r} = F_{x}\Delta x + F_{y}\Delta y + F_{z}\Delta z

where Δr\Delta \vec{r} represents the displacement between two points, r1r_{1} and r2r_{2}. Alternatively, the vector dot product can be solved following FΔr=FΔrcosθ\vec{F} \cdot \Delta \vec{r} = F\Delta r\cos \theta, where θ\theta is the angle between the two vectors.

If F\vec{F} and dr\mathrm{d}\vec{r} are parallel (θ(\theta = 0), then the force is acting in the same direction as the displacement and the force does maximum positive work. If the force is perpendicular to the displacement (θ=π2)(\theta = \frac{\pi}{2}), then the force does zero work. That is, the force is not responsible for the displacement and contributed no work to that displacement. If the force

is antiparallel to the displacement (θ=π)(\theta = \pi), then the force does maximum negative work (the force acts to counter the motion as much as it can).

Work is a scalar quantity. It has magnitude but no direction. Since work is calculated by a vector dot product between force and displacement, only the component of the force that is along the displacement vector matters for the work calculation. Thus, solving problems with energy can make the math much easier if you select the right coordinate system (e.g., Cartesian versus polar coordinates) when defining your force and displacement.

8.2 Work-Energy Theorem

Consider a net 1-D force FF that acts on a single particle in the xx direction. From Newton’s second law (in one dimension), we have:

F=md2xdt2=mdxdtdvdx=mvdvdxF = m \frac{\mathrm{d}^{2}x}{\mathrm{d}t^{2}} = m \frac{\mathrm{d}x}{\mathrm{d}t} \frac{\mathrm{d}v}{\mathrm{d}x} = mv \frac{\mathrm{d}v}{\mathrm{d}x}

using the chain rule (see Sample Problem 2-3 for more information). We can re-write the above as:

Fdx=mvdvFdx=12md(v2)=notethatd(v2)=2vdvFdx=d(12mv2)=misconstantFdx=dK\begin{aligned} F\mathrm{d}x &= mv\mathrm{d}v \\ F\mathrm{d}x &= \frac{1}{2} m\mathrm{d}(v^{2}) =\Rightarrow \mathrm{note} \mathrm{that} \mathrm{d}(v^{2}) = 2v\mathrm{d}v \\ F\mathrm{d}x &= \mathrm{d}\bigg(\frac{1}{2} mv^{2}\bigg) =\Rightarrow m \mathrm{is} \mathrm{constant} \\ F\mathrm{d}x &= \mathrm{d}K \end{aligned}

where KK corresponds to the kinetic energy of the system.

The work done by the force FF going from position x1x_{1} to x2x_{2} can be found by integrating both sides of the above equation:

x1x2F(x)dx=x1x2dKW2W1=K2K1\begin{aligned} \int_{x_{1}}^{x_{2}} F(x)\mathrm{d}x &= \int_{x_{1}}^{x_{2}} \mathrm{d}K \\ W_{2}- W_{1}&= K_{2}- K_{1} \end{aligned}
W(x1x2)=ΔKW(x_{1}\rightarrow x_{2}) = \Delta K

Equation 8.3 is the work-kinetic energy theorem.

Similarly, one can also define the work-kinetic energy theorem for rotation and torques. Recall from Chapter 7 that the net torque is:

τ=Iα=Id2θdt2=Idθdtdωdθ=Iωdωdθ\tau = I\alpha = I \frac{\mathrm{d}^{2}\theta}{\mathrm{d}t^{2}} = I \frac{\mathrm{d}\theta}{\mathrm{d}t} \frac{\mathrm{d}\omega}{\mathrm{d}\theta} = I\omega \frac{\mathrm{d}\omega}{\mathrm{d}\theta}

Now, torque is a vector quantity given by τ=r×F\vec{\tau} = \vec{r} \times \vec{F} . But work is a scalar quantity and the work done on a particle to move it from one position to another applies only to the component of the force in the direction of motion. If a force is perpendicular to the direction of motion, that force does no work. And if a force is parallel to the direction of motion, it does maximum work.

So if the path length in the direction of the force is ds=rs = rdθ\theta, then we can say that the work done by the force is:

dW=FsW = F_{s}ds=Fss =\Rightarrow F_{s} is the component parallel to the path ss

=Fsrdθ=subinds=rdθ= F_{s}r\mathrm{d}\theta =\Rightarrow \mathrm{sub} \mathrm{in} \mathrm{d}s = r\mathrm{d}\theta
=τdθ=τ=rFsbecauseFsrifFs//ds(e.g.,rds)= \tau \mathrm{d}\theta =\Rightarrow \tau = rF_{s}\mathrm{because} \vec{F}_{s}\perp \vec{r} \mathrm{if} \vec{F}_{s}// \mathrm{d}\vec{s} (\mathrm{e.g}., \vec{r} \perp \mathrm{d}\vec{s})

Combining this with our definition of torque from before, we get:

dW=τdθ=(Iωdωdθ)dθ=equationforτfromthesecondlaw\begin{aligned} \mathrm{d}W &= \tau \mathrm{d}\theta \\ &= \Bigg(I\omega \frac{\mathrm{d}\omega}{\mathrm{d}\theta} \Bigg)\mathrm{d}\theta =\Rightarrow \mathrm{equation} \mathrm{for} \tau \mathrm{from} \mathrm{the} \mathrm{second} \mathrm{law} \end{aligned}
=Iωdω=12Id(ω2)=notethatd(ω2)=2ωdω=d(12Iω2)=Iisconstant=dK\begin{aligned} &= I\omega \mathrm{d}\omega \\ &= \frac{1}{2} I\mathrm{d}(\omega ^{2}) =\Rightarrow \mathrm{note} \mathrm{that} \mathrm{d}(\omega ^{2}) = 2\omega \mathrm{d}\omega \\ &= \mathrm{d}\bigg(\frac{1}{2} I\omega ^{2}\bigg) =\Rightarrow I \mathrm{is} \mathrm{constant} \\ &= \mathrm{d}K \end{aligned}

Integrating both sides will give you the same answer as the linear case: W(θ1θ2)=ΔKW(\theta _{1}\rightarrow \theta _{2}) = \Delta K. So the work-kinetic energy theorem applies for both translation and rotation movement. The kinetic energy equations are slightly different, however.

K=12mv2=fortranslationK = \frac{1}{2} mv^{2}=\Rightarrow \mathrm{for} \mathrm{translation}
K=12Iω2=forrotationK = \frac{1}{2} I\omega ^{2}=\Rightarrow \mathrm{for} \mathrm{rotation}

8.3 Work in Different Frames

The work-kinetic energy theorem applies to all inertial frames (constant velocity) whether they are moving or stationary. So the change in work is the same within a stationary (S)(S) frame or in a moving frame SS^{\prime } (e.g., the centre-of-mass frame such as in Chapter 6).

Figure 8.1 show a particle starting from rest and moving under a constant force FF in a laboratory. This particle will have a constant acceleration aa due to this force. The work done to move this particle from point x1x_{1} to x2x_{2} in the laboratory frame (S)(S) is simply WS=FΔx=ΔKW_{S}= F\Delta x = \Delta K because all the motion is in 1-D.

Figure compares the standard 2D Cartesian axes for a rest frame and a moving frame.

Figure 8.1:The motion of a particle in two different inertial frames. The lab frame SS is stationary (red) and the second frame SS^{\prime } is moving at a constant velocity uu relative to the lab frame. A particle moves under a constant force FF with an acceleration aa in the lab frame. The work done to move that particle from points x1x_{1} to x2x_{2} in the lab frame is equal to the work done to move the particle in the moving inertial frame.

Now, consider what an observer in a moving frame, SS^{\prime } would measure for the work done by that force. Here, SS^{\prime } is moving at a constant velocity and is also an inertial frame. Because SS^{\prime } is moving at a constant velocity, the observer in SS^{\prime } would find the same acceleration as the observer in SS (e.g., ddt(v+v0)=dvdt\frac{\mathrm{d}}{\mathrm{d}t} (v + v_{0}) = \frac{\mathrm{d}v}{\mathrm{d}t} ). As a result, both the acceleration and force are unchanged in the moving frame. So

FS=FS=maF_{S}= F_{S^{\prime }}= ma

with the same value of aa for both frames.

If the force is constant (given in the question), then the work in the moving frame is WS=FΔxSW_{S^{\prime }}= \vec{F}\Delta \vec{x}_{S^{\prime }}, where ΔxS\Delta \vec{x}_{S^{\prime }} is the displacement in the moving frame. Note that since the motion still takes place in 1-D we can drop vectors (if there are more dimensions, you just need to break up the movement by each coordinate).

For the displacement, ΔxS\Delta \vec{x}_{S^{\prime }}, we need to know how far the particle travels in time Δt\Delta t. For a system with constant acceleration (see Chapters 1 and 2), the displacement Δx=12at2+vit\Delta x = \frac{1}{2} at^{2}+v_{i}t, where viv_{i} is the initial velocity of the system. While the particle is initially at rest in the stationary frame, from the perspective of the moving frame, the particle does not start stationary. The moving frame has a velocity of uı^-u\hat{\imath} relative to the lab frame. That means that the moving frame would see the particle as having an initial speed of uı^u\hat{\imath}. So we can say that vi=uv_{i}= u and the displacement is:

Δx=12at2+vit=12at2+ut\Delta x = \frac{1}{2} at^{2}+ v_{i}t = \frac{1}{2} at^{2}+ ut

Taking our equations for FF and Δx\Delta x in the moving frame, the work done by the force is

ΔW=FΔx=(ma)(12at2+ut)=12m[(at)2+2uat]=12m[(at)2+2uat+u2u2]=add and subtract u2 (same as adding zero)=12m[(at+u)2u2]=recall that (a+b)2=a2+2ab+b2=12m[vf2u2]=for constant acceleration, vf=at+u=12m[vf2vi2]=u is just the initial velocity, vi=KfKi=ΔK\begin{aligned} \Delta W &= F\Delta x \\ &=(ma)\left(\frac12at^2+ut\right)\\ &=\frac12m\left[(at)^2+2uat\right]\\ &=\frac12m\left[(at)^2+2uat+u^2-u^2\right]=\Rightarrow\mathrm{add}\ \mathrm{and}\ \mathrm{subtract}\ u^{2}\ (\mathrm{same}\ \mathrm{as}\ \mathrm{adding}\ \mathrm{zero})\\ &=\frac12m\left[(at+u)^2-u^2\right]=\Rightarrow\mathrm{recall}\ \mathrm{that}\ (a+b)^{2}=a^{2}+2ab+b^{2}\\ &=\frac12m\left[v_f^2-u^2\right]=\Rightarrow\mathrm{for}\ \mathrm{constant}\ \mathrm{acceleration},\ v_{f}=at+u\\ &=\frac12m\left[v_f^2-v_i^2\right]=\Rightarrow u\ \mathrm{is}\ \mathrm{just}\ \mathrm{the}\ \mathrm{initial}\ \mathrm{velocity},\ v_{i}\\ &=K_f-K_i\\ &=\Delta K \end{aligned}

where KfK_{f} is the final kinetic energy and KiK_{i} in the initial kinetic energy.

So while the values of WW and KK as measured in the two frames (stationary and moving) may be different, the requirement that ΔW=ΔK\Delta W = \Delta K holds in both frames. Again, this is only the case for inertial frames. In non-inertial frames (e.g., rotating or accelerating frames), the net force will include fictitious forces due to the non-inertial frame and the measured accelerations would be different (see Chapters 4 and 5).

8.4 Gravity

8.4.1 Simple Approximation

Near the Earth’s surface, we often describe the gravitational force as Fg=mg\vec{F}_{g}= m\vec{g}, where g\vec{g} is a constant vector that points down vertically and has a constant magnitude.

Consider the case where the position of a heavy box of mass mm changes y1y_{1} to y2y_{2} in vertical height and that both positions y2y_{2} and y1y_{1} are near the Earth’s surface. Work is done by gravity as the box moves by this displacement. The vector describing the displacement of

the box is Δy=(y2y1)ȷ^\Delta \vec{y} = (y_{2}-y_{1})\hat{\jmath} , whereas the gravitational force is Fg=mgȷ^\vec{F}_{g}= -mg\hat{\jmath} , which is constant. Taking the equation for work with a constant force, the work is:

ΔW=FgΔy\Delta W = \vec{F}_{g}\cdot \Delta \vec{y}
=(mgȷ^)(y2y1)ȷ^= (-mg\hat{\jmath}) \cdot (y_{2}- y_{1})\hat{\jmath}
=mg(y2y1)=ȷ^ȷ^=1= -mg(y_{2}- y_{1}) =\Rightarrow \hat{\jmath} \cdot \hat{\jmath} = 1

Remember, this is the work done by gravity. So if a box is lifted upward (y2>y1)(y_{2}> y_{1}), gravity acts against the displacement and W<0W < 0. If the box is lowered (y2<y1)(y_{2}< y_{1}), gravity acts with (helps) the displacement and W>0W > 0. And if y2=y1y_{2}= y_{1} then WW = 0 (no work is done by gravity).

8.4.2 General Equation

In general, the true form of the gravitational force is:

Fg=GMmr2r^\vec{F}_{g}= - \frac{GMm}{r^{2}} \hat{r}

where GG is the gravitational constant of 6.67×10116.67 \times 10^{-11} N m2kg2,M\mathrm{m}^{2}\mathrm{kg}^{-2}, M is the mass of the object producing the gravitational field, mm is the mass of an object being accelerated in the gravitational field, and rr is the distance between the centers of the two objects. Thus, the true form for the acceleration due to gravity is given by:

g=GMr2r^\vec{g} = - \frac{GM}{r^{2}} \hat{r}

Note that the acceleration due to gravity always points toward the centre of the source of the gravitational field (points radially inward).

The force of gravity is a radial force with no azimuthal (angle) dependence. That means that any point that has the same radial distance (r)(|\vec{r}|) will have the same magnitude of gravity g|\vec{g}|. We often describe gravity as a gravitational field, a sphere of influence where any object with a mass mm will be subjected to a gravitational force. The magnitude of the gravitational field changes as a function of radial distance. For example, Figure 8.2 shows a cartoon of the Earth with two different vectors, r1\vec{r}_{1} and r2\vec{r}_{2}. Their magnitudes of gravitational acceleration are:

g1=GMr12andg2=GMr22|\vec{g}_{1}| = \frac{GM}{r_{1}^{2}} \mathrm{and} |\vec{g}_{2}| = \frac{GM}{r_{2}^{2}}
Figure shows two different radial orbits around the Earth.

Figure 8.2:A cartoon of the Earth with two different vectors, r1\vec{r}_{1} and r2\vec{r}_{2}. Each vector also has a circle with corresponding radii of r1r_{1} and r2r_{2}. Every point on the r1r_{1} circle will have the same gravitational field magnitude and similarly, every point on the r2r_{2} circle will have the same gravitational field magnitude.

Since r2>r1,g1>g2r_{2}> r_{1}, |\vec{g}_{1}| > |\vec{g}_{2}|. But any point on a sphere with radius r1r_{1} around the Earth will have the same magnitude of acceleration due to gravity (e.g., the circles in Figure 8.2), and likewise for all the points on a sphere with radius r2r_{2}. You can think of gravity as a sphere of influence, where any point that has the same distance from the centre of the Earth has the same magnitude of g|\vec{g}|.

Note that the direction of gravity will be different depending on where you are, because the force always points inward toward the centre of the Earth (in its true form, gravity is not vertical, but radial). For very small distances and positions near the Earth’s surface, you can still assume a vertical direction and constant magnitude for a frame at that surface.

What is the work done by gravity using this general equation?

Well, consider going from r1r_{1} to r2r_{2} as shown in Figure 8.2.

W(r1r2)=r1r2Fdr=forceisnotconstant=r1r2(GMmr2)r^dr=usetheequationfortheforceofgravity=GMmr1r2(1r2r^)(drr^)=dr=drr^=GMmr1r2(1r2dr)r^r^=a^a^=1foranyunitvector=GMmr1r21r2dr=GMm(1rr1r2)=GMmr2GMmr1\begin{aligned} W(r_{1}\rightarrow r_{2}) &= \int_{r_{1}}^{r_{2}} \vec{F} \cdot \mathrm{d}\vec{r} =\Rightarrow \mathrm{force} \mathrm{is} \mathrm{not} \mathrm{constant} \\ &= \int_{r_{1}}^{r_{2}} \bigg(- \frac{GMm}{r^{2}} \bigg)\hat{r} \cdot \mathrm{d}\vec{r} =\Rightarrow \mathrm{use} \mathrm{the} \mathrm{equation} \mathrm{for} \mathrm{the} \mathrm{force} \mathrm{of} \mathrm{gravity} \\ &= -GMm\int_{r_{1}}^{r_{2}} \bigg(\frac{1}{r^{2}} \hat{r}\bigg) \cdot (\mathrm{d}r\hat{r}) =\Rightarrow \mathrm{d}\vec{r} = \mathrm{d}r\hat{r} \\ &= -GMm\int_{r_{1}}^{r_{2}} \bigg(\frac{1}{r^{2}} \mathrm{d}r\bigg)\hat{r} \cdot \hat{r} =\Rightarrow \hat{a} \cdot \hat{a} = 1 \mathrm{for} \mathrm{any} \mathrm{unit} \mathrm{vector} \\ &= -GMm\int_{r_{1}}^{r_{2}} \frac{1}{r^{2}} \mathrm{d}r \\ &= -GMm\bigg(- \frac{1}{r} \bigg|_{r_{1}}^{r_{2}} \bigg) \\ &= \frac{GMm}{r_{2}} - \frac{GMm}{r_{1}} \end{aligned}

Note that if r2>r1,W<0r_{2}> r_{1}, W < 0 as we would expect (e.g., you are doing work against gravity to move an object further away). You may recognize GMmr- \frac{GMm}{r} as the gravitational potential energy. We will discuss potential energies in more detail in Section 8.6.

8.4.3 Escape velocity

The gravitational force follows an inverse square ( 1r2)\frac{1}{r^{2}}) law. So at very large distances from the source of the gravitational field, the gravitational force goes to zero and the work necessary to move a particle also goes to zero (if there is no force, there is no work).

Consider an object that is on the surface of Earth and is launched so that it reaches a very large distance away (assume infinity). Due to Earth’s gravitational field, the object will feel a force that opposes its motion to leave. Gravity will be doing negative work and the kinetic energy of the object will decrease. What speed is needed for this object to just reach infinity? Assume Earth’s atmosphere does not affect its motion.

To solve this problem, we will use the work-kinetic energy theorem (Equation (8.3)).

W(r1r2)=ΔK=12mv2212mv12W(r_{1}\rightarrow r_{2}) = \Delta K = \frac{1}{2} mv_{2}^{2}- \frac{1}{2} mv_{1}^{2}

We just solved for the work to move an object between two radii in a gravitational field. We start with Earth’s surface (r1=RE)(r_{1}= R_{E}) and we end very far away (r2=)(r_{2}= \infty). That means that:

W(r1r2)=GMmr2GMmr1=0GmMEREW(r_{1}\rightarrow r_{2}) = \frac{GMm}{r_{2}} - \frac{GMm}{r_{1}} = 0 - \frac{GmM_{E}}{R_{E}}

where RER_{E} is the radius of the Earth, MEM_{E} is the mass of the Earth, and mm is the mass of our object being moved. For kinetic energy, v2v_{2} = 0 because the object just reaches infinity. As such:

W(r1r2)=12mv2212mv12GmMERE=012mv12v12=2GMERE\begin{aligned} W(r_{1}\rightarrow r_{2}) &= \frac{1}{2} mv_{2}^{2}- \frac{1}{2} mv_{1}^{2} \\ - \frac{GmM_{E}}{R_{E}} &= 0 - \frac{1}{2} mv_{1}^{2} \\ v_{1}^{2}&= \frac{2GM_{E}}{R_{E}} \end{aligned}
vesc=2GMERE.v_{esc}=\sqrt{\frac{2GM_E}{R_E}}.

Equation 8.9 describes the escape velocity and for Earth, which is roughly 11 km s1\mathrm{s}^{-1}. The escape velocity is the minimum speed for rockets and satellites to leave Earth’s surface and travel great distances away.

Note that an object starting from rest at a great distance from the Earth will hit the Earth at a speed equivalent to the escape velocity. This converse situation is true because gravity is a conservative force, which we will discuss in the next section.

8.5 Conservative Forces

Conservative forces are a class of forces that depend only on position. These forces are also ones where energy is conserved. Common examples of conservative forces are gravity, the spring force, and the electric force. Conservative forces must meet the following criteria:

  1. A conservative force does no total work on an object during a round trip.

  2. The work done by a conservative force is independent of the path taken between two points.

The first requirement states:

W(r1r1)=Fdr=0W(r_{1}\rightarrow r_{1}) = \oint \vec{F} \cdot \mathrm{d}\vec{r} = 0

where \oint indicates an integral over a closed loop. For example, if you measure the work between r1r2r_{1}\rightarrow r_{2} and then r2r1r_{2}\rightarrow r_{1}, the work function would be:

W(r1r2r1)=r1r2Fdr+r2r1FdrW(r_{1}\rightarrow r_{2}\rightarrow r_{1}) = \int_{r_{1}}^{r_{2}} \vec{F} \cdot \mathrm{d}\vec{r} + \int_{r_{2}}^{r_{1}} \vec{F} \cdot \mathrm{d}\vec{r}

For a conservative force, that equation would equal zero.

Now consider the case of gravity,

r1r2Fdr=GMmr2GMmr1r2r1Fdr=GMmr1GMmr2\begin{aligned} \int_{r_{1}}^{r_{2}} \vec{F} \cdot \mathrm{d}\vec{r} &= \frac{GMm}{r_{2}} - \frac{GMm}{r_{1}} \\ \int_{r_{2}}^{r_{1}}\vec{F} \cdot \mathrm{d}\vec{r} &= \frac{GMm}{r_{1}} - \frac{GMm}{r_{2}} \end{aligned}

If you add those two segments, you indeed get WW = 0. This is true for any number of stops in the closed loop. As long as your starting and final positions are the same, you will get WW = 0 for a conservative force.

The second requirement states that the total work done to move an object between two points only depends on the initial and final positions. How you get from point one to point two doesn’t matter. Figure 8.3 shows two paths that connect points r1r_{1} and r2r_{2}. The work done by a conservative force will be the same no matter the path chosen.

Figure shows two paths between the same two points, one linear and one wandering.

Figure 8.3:Comparison of two paths between points r1r_{1} and r2r_{2}. For a conservative force, the work done to go from r1r_{1} to r2r_{2} is the same for both paths, even though the paths are very different.

And of course, if you go from r1r_{1} to r2r_{2} and then from r2r_{2} back to r1r_{1}, the total work is zero (first criterion) no matter which path you take in either case (e.g., Path I from r1r_{1} to r2r_{2} and then Path II from r2r_{2} back to r1)r_{1}).

Note that forces like friction are not conservative forces. First, friction doesn’t depend on position. Second, friction removes energy from a system. Third, the work done by friction in a closed loop is not zero. For example, consider a hockey puck moving in a circle of radius RR on a rough horizontal surface that has friction. The friction force on the hockey puck is f=μKmgθ^\vec{f} = \mu _{K}mg\hat{\theta} , and the puck moves so that it is always antiparallel (180)(180^{\circ}) to the displacement. So Wf=fΔd=μKmg(2πR)W_{f}= -f\Delta d = -\mu _{K}mg(2\pi R) for a closed loop. Thus, WfW_{f}\not = 0.

8.5.1 Identifying Conservative Forces

A conservative force can be identified mathematically using the following condition:

×F=0\vec{\nabla} \times \vec{F} = 0

Note that ×F\vec{\nabla} \times \vec{F} is a vector cross product called the curl of the vector F\vec{F} . The \vec{\nabla} symbol is a vector differential operator sometimes called the del or nabla operator. In Cartesian coordinates, it has the form of:

=xı^+yȷ^+zk^\vec{\nabla} = \frac{\partial}{\partial x} \hat{\imath} + \frac{\partial}{\partial y} \hat{\jmath} + \frac{\partial}{\partial z} \hat{k}

where \partial indicates the partial derivative. For partial derivatives, you ignore any other variable. For example, xf(y)\frac{\partial}{\partial x} f(y) = 0 because xx is not present in the function (you treat yy as a constant for a partial derivative with respect to x)x). For \vec{\nabla} in other coordinate systems, see Appendix A.5.

The curl of A\vec{A} (in Cartesian coordinates) is then given by the following matrix.

×A=ı^ȷ^k^xyzAxAyAz=(yAzzAy)ı^+(zAxxAz)ȷ^+(xAyyAx)k^\begin{aligned} \vec{\nabla} \times \vec{A} &= \begin{vmatrix} \hat{\imath} & \hat{\jmath} & \hat{k} \\ \frac{\partial}{\partial x} & \frac{\partial}{\partial y} & \frac{\partial}{\partial z} \\ A_{x} & A_{y} & A_{z} \end{vmatrix} \\ &= \Bigg(\frac{\partial}{\partial y} A_{z}- \frac{\partial}{\partial z} A_{y}\Bigg)\hat{\imath} + \Bigg(\frac{\partial}{\partial z} A_{x}- \frac{\partial}{\partial x} A_{z}\Bigg)\hat{\jmath} + \Bigg(\frac{\partial}{\partial x} A_{y}- \frac{\partial}{\partial y} A_{x}\Bigg)\hat{k} \end{aligned}

A conservative force has ×F\vec{\nabla} \times \vec{F} = 0 by definition. We will discuss why in Chapter 8.6.

8.5.2 Example Conservative Forces

8.6 Potential Energy

The potential energy represents the energy of a system based on its position or configuration. It represents the capacity of the system to do work,

ΔU=ΔWcon\Delta U = -\Delta W_{con}

where ΔWcon\Delta W_{con} is the work done by a conservative force. More formally,

U(r1r2)=r1r2Fdr=Wcon(r1r2)U(r_{1}\rightarrow r_{2}) = -\int_{r_{1}}^{r_{2}} \vec{F} \cdot \mathrm{d}\vec{r} = -W_{con}(r_{1}\rightarrow r_{2})

Potential energy is associated with conservative forces only. Consider a heavy box. If you lift that box upward, the work done by gravity is negative (gravity opposes the motion), but you increase the potential energy of the box because work is being done against gravity (W<0)(W < 0). If you lower that box or let go, then gravity is doing positive work on the box (W>0)(W > 0) and it will have a decrease in potential energy.

Let’s look at the gravitational potential energy between positions r1r_{1} and r2r_{2}.

U(r1r2)=Wcon(r1r2)=r1r2Fdr=r1r2(GMmr2r^)(drr^)=r1r2GMmr2dr=GMmrr1r2=GMmr2+GMmr1.\begin{aligned} U(r_1\to r_2) &=-W_{con}(r_1\to r_2)\\ &=-\int_{r_1}^{r_2}\vec{F}\cdot\mathrm{d}\vec{r}\\ &=-\int_{r_1}^{r_2}\left(-\frac{GMm}{r^2}\hat{r}\right)\cdot(\mathrm{d}r\,\hat{r})\\ &=\int_{r_1}^{r_2}\frac{GMm}{r^2}\,\mathrm{d}r\\ &=\left.-\frac{GMm}{r}\right|_{r_1}^{r_2} =-\frac{GMm}{r_2}+\frac{GMm}{r_1}. \end{aligned}

In general, the gravitational potential energy is measured between two points. It is a relative energy. You will want to set a convenient reference point. For example, we can set r1=r_{1}= \infty, where there would be no contribution from the force, such that:

U=GMmr(comparedtoinfinity)U = - \frac{GMm}{r} (\mathrm{compared} \mathrm{to} \mathrm{infinity})

For gravity problems near Earth’s surface, setting UU = 0 at the surface is often convenient.

The potential energy for the spring force going from x1x_{1} to x2x_{2} is:

U(x1x2)=x1x2(kxx^)(dxx^)=x1x2kxdx=12kx2x1x2=12kx2212kx12U(x_{1}\rightarrow x_{2}) = -\int_{x_{1}}^{x_{2}} (-kx\hat{x}) \cdot (\mathrm{d}x\hat{x}) = \int_{x_{1}}^{x_{2}} kx\mathrm{d}x = \frac{1}{2} kx^{2}\Big|_{x_{1}}^{x_{2}} = \frac{1}{2} kx_{2}^{2}- \frac{1}{2} kx_{1}^{2}

Once again, we want to set a convenient initial value like x1x_{1} = 0 (the equilibrium position), so that the potential energy of a spring is simply U=12kx2U = \frac{1}{2} kx^{2} relative to that point.

8.7 Conservation of Energy

The work-kinetic energy theorem states that ΔW=ΔK\Delta W = \Delta K. That is, the total work on a system by a force is equal to the change in the kinetic energy. The total work is the sum of work by conservative forces (ΔWcon)(\Delta W_{con}) and the work by non-conservative forces (ΔWnc)(\Delta W_{nc}):

ΔW=ΔK\Delta W = \Delta K
ΔWcon+ΔWnc=ΔK=ΔW=ΔWcon+ΔWnc\Delta W_{con}+ \Delta W_{nc}= \Delta K =\Rightarrow \Delta W = \Delta W_{con}+ \Delta W_{nc}
ΔWnc=ΔKΔWcon\Delta W_{nc}= \Delta K - \Delta W_{con}
ΔWnc=ΔK+ΔU=ΔWcon=ΔU\Delta W_{nc}= \Delta K + \Delta U =\Rightarrow \Delta W_{con}= -\Delta U

Setting ΔWnc=ΔE\Delta W_{nc}= \Delta E, or the change in mechanical energy (non-conservative work), we get:

ΔE=Δ(K+U)\Delta E = \Delta (K + U)

For small times dtt, you can say that dE=d(K+U)E = \mathrm{d}(K+U). Integrating these functions then gives

E=K+U.E = K + U.

In the absence of non-conservative forces (e.g., if all forces acting on a system are conservative), then ΔWnc\Delta W_{nc} = 0 and ΔE\Delta E = 0 such that we get Δ(K+U)\Delta (K + U) = 0 or K+UK + U = constant. This is the conservation of energy. When energy is conserved, ΔK=ΔU\Delta K = -\Delta U or the change in kinetic energy directly corresponds to a change in potential energy. If kinetic energy increases, then potential energy decreases and vice versa.

8.8 Application of Potential Energy

A conservative force can also be written in terms of the potential energy,

F=U=(Uxı^+Uyȷ^+Uzk^)\vec{F} = -\vec{\nabla}U = -\Bigg(\frac{\partial U}{\partial x} \hat{\imath} + \frac{\partial U}{\partial y} \hat{\jmath} + \frac{\partial U}{\partial z} \hat{k}\Bigg)

for Cartesian coordinates (see Appendix A.5 for other coordinate systems). The \vec{\nabla} operator in this context means the gradient of UU.

We can use this definition of a conservative force to show that U(r1r2)=W(r1r2)U(r_{1}\rightarrow r_{2}) = -W(r_{1}\rightarrow r_{2}).

W(r1r2)=r1r2Fdr=r1r2(U)dr=substituteinourscalarfield=r1r2dUr=onlythecomponentalongthepathisnonzero=(Urr1r2)=onlytheendpointsmatterforconservativeforces=U(r1r2)\begin{aligned} W(r_{1}\rightarrow r_{2}) &= \int_{r_{1}}^{r_{2}} \vec{F} \cdot \mathrm{d}\vec{r} \\ &= \int_{r_{1}}^{r_{2}}(-\vec{\nabla}U) \cdot \mathrm{d}\vec{r} =\Rightarrow \mathrm{substitute} \mathrm{in} \mathrm{our} \mathrm{scalar} \mathrm{field} \\ &= -\int_{r_{1}}^{r_{2}} \mathrm{d}U_{r}=\Rightarrow \mathrm{only} \mathrm{the} \mathrm{component} \mathrm{along} \mathrm{the} \mathrm{path} \mathrm{is} \mathrm{non-zero} \\ &= -\Big(U_{r}\Big|_{r_{1}}^{r_{2}}\Big) =\Rightarrow \mathrm{only} \mathrm{the} \mathrm{end} \mathrm{points} \mathrm{matter} \mathrm{for} \mathrm{conservative} \mathrm{forces} \\ &= -U(r_{1}\rightarrow r_{2}) \end{aligned}

Exactly as we expect. Thus, the potential energy of a conservative force satisfies F=U\vec{F} = -\vec{\nabla}U.

Moreover, ×F\vec{\nabla} \times \vec{F} = 0 for a conservative force. We can substitute in F=U\vec{F} = -\vec{\nabla}U,

×(U)=ı^ȷ^k^xyzUxUyUz\vec{\nabla} \times (-\vec{\nabla}U) = \begin{vmatrix} \hat{\imath} & \hat{\jmath} & \hat{k} \\ \frac{\partial}{\partial x} & \frac{\partial}{\partial y} & \frac{\partial}{\partial z} \\ \frac{\partial U}{\partial x} & \frac{\partial U}{\partial y} & \frac{\partial U}{\partial z} \end{vmatrix}
=(yUzzUy)ı^(zUxxUz)ȷ^(xUyyUx)k^= -\Bigg(\frac{\partial}{\partial y} \frac{\partial U}{\partial z} - \frac{\partial}{\partial z} \frac{\partial U}{\partial y} \Bigg)\hat{\imath} - \Bigg(\frac{\partial}{\partial z} \frac{\partial U}{\partial x} - \frac{\partial}{\partial x} \frac{\partial U}{\partial z} \Bigg)\hat{\jmath} - \Bigg(\frac{\partial}{\partial x} \frac{\partial U}{\partial y} - \frac{\partial}{\partial y} \frac{\partial U}{\partial x} \Bigg)\hat{k}
=(2Uyz2Uzy)ı^(2Uzx2Uxz)ȷ^(2Uxy2Uyx)k^= -\Bigg(\frac{\partial ^{2}U}{\partial y\partial z} - \frac{\partial ^{2}U}{\partial z\partial y} \Bigg)\hat{\imath} - \Bigg(\frac{\partial ^{2}U}{\partial z\partial x} - \frac{\partial ^{2}U}{\partial x\partial z} \Bigg)\hat{\jmath} - \Bigg(\frac{\partial ^{2}U}{\partial x\partial y} - \frac{\partial ^{2}U}{\partial y\partial x} \Bigg)\hat{k}
=0ı^+0ȷ^+0k^=0= 0\hat{\imath} + 0\hat{\jmath} + 0\hat{k} = 0

Note for the above we are assuming that UU is twice continuously differentiable. If UU can be differentiated twice, then its partial derivatives are independent of the order and all terms cancel (e.g, 2Uyz=2Uzy)\frac{\partial ^{2}U}{\partial y\partial z} = \frac{\partial ^{2}U}{\partial z\partial y}).

For a potential, UU, there can be points where U=F-\vec{\nabla}U = \vec{F} = 0. Mathematically, these points are located where the derivative of the potential is zero and correspond to points of local maxima or local minima. Figure 8.5) shows a sketch of a potential with a local maximum and local minimum. These locations are also known as equilibrium points or saddle points.

Figure shows a simple graph of a cubic-shaped function with local maximum and minimum points labeled to demonstrate equilibrium points.

Figure 8.5:Example potential with a local maximum and local minimum.

A local minimum is a stable equilibrium point. At the minimum, if a particle is slightly perturbed, it wouldn’t really go anywhere. The particle will feel a force that just brings it back to the minimum saddle point. Recall that the force is the negative derivative of the potential, so if you perturb the particle to a lower xx value, the potential has a negative slope and the force will be positive back toward the saddle point. And if you perturb the particle to a higher xx value, the potential has a positive slope and the force will be negative back toward the saddle point. So for a small shift in position, your particle more or less stays at the saddle point.

At the local maximum saddle point, however, a slight perturbation will have a huge effect on the particle’s motion. If you slightly perturb the particle to a lower xx value, the potential has a positive slope so the force will be negative toward even more negative xx values. (Similar case if you perturb the particle to a higher xx value). So a slight perturbation at the maximum of a potential will cause the system to be unstable and move away from that position.

8.9 Summary

8.10 Practice Problems

See Appendix C for answers to the practice problems.