1. Introduction
  2. Electric Potential Energy Differences ( Ξ” P E \Delta PE )
    1. Problem – Uniform Field
    2. Problem – Radial Field
  3. Electric potential difference Ξ” V \Delta V
    1. Problem – Uniform Field
    2. Problem – Radial Field
  4. E = βˆ’ βˆ‡ V \mathbf{E} = -\boldsymbol{\nabla}V
    1. Example
    2. Example
    3. Example
  5. V V for a point charge
    1. Example
    2. Problem
  6. V V for of a Group of Charges
    1. Example
  7. W W for a Group of Charges
    1. Example – Charges on x x –Axis
    2. Problem – Charges at Corners of Triangle

In sections 2. and 3. an introduction to electric potential difference, Ξ” V \Delta V is given using the notation used in PHYS 260 and using problems at that level.

In section 4., V V is derived based on vector field concepts following the notation of Griffiths.

The chapter on potential in your PHYS 260 textbook and Griffiths 2.3 and 2.4 are recommended as references. An additional reference is guide03.pdf.

The potential energy of an object increases when you do a positive amount of work on it. For example, if you lift a mass from the floor, you increase its potential energy. The work done on an object changes its potential energy, and this change is represented by Ξ” P E \Delta PE .

Mathematically, the work done by a force F \mathbf{F} in moving an object from position a a to position b b along a line l l is

W a β†’ b = ∫ a b F β‹… d l W_{a\rightarrow b}=\int_a^b \mathbf{F}\cdot d\mathbf{l}

and this work changes the potential energy of an object according to

W a β†’ b = P E b βˆ’ P E a ≑ Ξ” P E W_{a\rightarrow b} = PE_b-PE_a \equiv \Delta PE

where the symbol ≑ \equiv is used to indicate that Ξ” P E \Delta PE is defined to be the final potential at b b minus the initial potential at a a .

If a force is always perpendicular to the direction of movement, the work due to that force is zero.

When the force on an object does not change when it is moved a distance L L from a a to b b along a straight line, and the force vector is aligned with the path of movement, then

W a β†’ b = ∫ a b F β‹… d l = ( Β± ) ∣ F ∣ L W_{a\rightarrow b}=\int_a^b \mathbf{F}\cdot d\mathbf{l}=(\pm)|\mathbf{F}|L

where L L is positive; the + + sign is used for a force that is in the direction of movement and the βˆ’ - sign is used for a force that is in the opposite direction of movement. (You should know how to derive this.) For example, if you lift a mass m m upwards by a distance L L , the force you exert is in the same direction of movement, so you do a work of m g L mgL . The gravitational force on the mass is in the opposite direction of movement, so the work done by the gravitational force is βˆ’ m g L -mgL .

One of the most common difficulties in calculating work and energy is getting the correct sign for the answer. The following two problems have questions that ensure that you are able to predict the correct sign of work and changes in potential energy.

The following diagram shows a region of space where the electric field is constant and has a value of 3 3  N/C.

1. You place a charge of + 3 +3  C at point A A . What happens to that charge when it is released?

2. You move a charge of + 3 +3  C from A A to B B . (a) How much work did you do? (b) How much work was done by the electric field? (c) By how much has the potential energy of the charge changed?

3. You place a charge of βˆ’ 3 -3  C at point A A . What happens to that charge when it is released?

4. A charge of βˆ’ 3 -3  C is moved from A A to B B . How much work did you do? (b) How much work was done by the electric field? (c) By how much has the potential energy of the charge changed?

5. You move a charge of + 3 +3  C straight downward from A A to C C . (a) How much work did you do? (b) How much work was done by the electric field? (c) By how much has the potential energy of the charge changed?

6. If you move a charge of βˆ’ 3 -3  C from A A to C C but deviate from a straight line, will your answers to the previous problem change? If no, explain why. If yes, provide new answers.

In the previous problem, a charge was moved in a region of space where the electric field was constant and so the calculation of work did not require integration. In this problem, the electric field is not constant and so the calculation of work requires integration.

There is a charge of βˆ’ 6 -6  C at the origin. Some electric field lines for this charge are shown. To simplify the math, use k = 9 β‹… 1 0 9  N β‹… m 2 / C 2 k=9\cdot 10^9\text{ N}\cdot\text{m}^2/\text{C}^2 .

1. You move a charge of + 3  C +3\text{ C} from A A to B B . (a) How much work did you do? (b) How much work was done by the electric field? (c) By how much has the potential energy of the moved charge changed?

2. You move a charge of βˆ’ 3 -3  C from A A to B B . (a) How much work did you do? (b) How much work was done by the electric field? (c) By how much has the potential energy of the moved charge changed?

3. You move a charge of βˆ’ 3 -3  C from B B to C C along the dotted line. (a) How much work did you do? (b) How much work was done by the electric field? (c) By how much has the potential energy of the moved charge changed?

4. You move a charge of βˆ’ 3 -3  C from C C to B B but deviate from the dotted line. (a) How much work did you do? (b) How much work was done by the electric field? (c) By how much has the potential energy of the moved charge changed?

In the previous section, we considered moving an arbitrary amount of charge (either positive or negative) from point a a to point b b and computed its change in potential energy Ξ” P E \Delta PE .

An electric potential difference Ξ” V \Delta V is defined to be the change in electric potential energy of a (positive by convention) test charge when it is moved from point a a to point b b divided by the magnitude of the test charge.

As a result, the only difference between the Ξ” P E \Delta PE calculations performed previously and Ξ” V \Delta V calculations is that we first compute Ξ” P E \Delta PE for a + 1 +1  C charge. To get Ξ” V \Delta V , we simply divide by Ξ” P E \Delta PE by + 1 +1  C.

The definition of electric potential is similar to the definition of electric field in that they both involve the consideration of a test charge. That is, the electric field is the force on a test charge divided by the magnitude of the test charge:

E = F q o \mathbf{E} = \frac{\mathbf{F}}{q_o}

A change in potential is the change in potential of a test charge divided by the magnitude of the test charge’s charge:

Ξ” V = Ξ” P E q o \Delta V = \frac{\Delta PE}{q_o}

The advantage of using changes in electric potential, Ξ” V \Delta V , as opposed to changes in electric potential energy, Ξ” P E \Delta PE , of a specific amount of charge is that once the electric potential difference Ξ” V \Delta V is known for a test charge, the change in potential energy for an arbitrary amount of charge Q Q can be computed by simply multiplying Ξ” V \Delta V and Q Q . This is similar to the advantage of the electric field. If we know the electric field at a given point, we can find the force on an arbitrary charge Q Q by multiplying E \mathbf{E} and Q Q .

The following diagram shows a region of space where the electric field is constant and has a value of 3 3  N/C.

1. What is the difference in potential Ξ” V = V B βˆ’ V A \Delta V = V_B-V_A ?

2. What is the difference in potential Ξ” V = V B βˆ’ V C \Delta V = V_B-V_C ?

3. You move a charge of + 3 +3  C from A A to B B . By how much has the electric potential energy of the moved charge changed?

4. You move a charge of βˆ’ 3 -3  C from A A to B B . By how much has the electric potential energy of the moved charge changed?

5. You move a charge of βˆ’ 3 -3  C from B B to C C . By how much has the electric potential energy of the moved charge changed?

There is a charge of βˆ’ 6 -6  C at the origin. Some electric field lines for this charge are shown. To simplify the math, use k = 9 β‹… 1 0 9 k=9\cdot 10^9  N β‹… \cdot m 2 ^2 /C 2 ^2 .

1. What is difference in potential Ξ” V = V B βˆ’ V A \Delta V = V_B-V_A .

2. What is difference in potential Ξ” V = V C βˆ’ V A \Delta V = V_C-V_A .

3. You move a charge of βˆ’ 3 -3  C from A A to B B . By how much has the potential energy of the moved charge changed?

4. You move a charge of βˆ’ 3 -3  C from B B to C C . By how much has the potential energy of the moved charge changed?

In the previous section, the potential difference between two points were computed for an electric field that was constant and a field due to a point charge at the origin. It was noted that Ξ” V = ∫ a b E β‹… d l \Delta V=\int_a^b\mathbf{E}\boldsymbol{\cdot} d\mathbf{l} was independent of the integration path chosen between a a and b b

In this section, we show that given information about how V V changes at a point, we can compute E \mathbf{E} at that point.

Recall that the gradient of a scalar field f f gives a vector field. That is, we can associate a vector field U \mathbf{U} with a scalar field by performing the operation

U = βˆ‡ f \mathbf{U}=\boldsymbol{\nabla}f

For f f in cartesian coordinates, we would compute U \mathbf{U} using

U = βˆ‡ f ( x , y , z ) = βˆ‚ f βˆ‚ x x ^ + βˆ‚ f βˆ‚ y y ^ + βˆ‚ f βˆ‚ z z ^ \mathbf{U}= \boldsymbol{\nabla}f(x,y,z)=\frac{\partial f}{\partial x}\mathbf{\hat{x}}+\frac{\partial f}{\partial y}\mathbf{\hat{y}}+\frac{\partial f}{\partial z}\mathbf{\hat{z}}

and for f f in cylindrical or spherical coordinates, the equations for βˆ‡ f \boldsymbol{\nabla}f are given on the second–to last page of Griffiths.

For example, in HW #1, you showed that βˆ‡ ( 1 ∣ r βˆ’ r β€² ∣ ) = βˆ’ ∣ r βˆ’ r β€² ∣ 3 ∣ r βˆ’ r β€² ∣ 3 \boldsymbol{\nabla}\left(\frac{1}{|\mathbf{r}-\mathbf{r}'|}\right)=\displaystyle -\frac{\phantom{|}\mathbf{r}-\mathbf{r}'\phantom{|^3}}{|\mathbf{r}-\mathbf{r}'|^3} by first writing f = 1 / ∣ r βˆ’ r β€² ∣ f=1/|\mathbf{r}-\mathbf{r}'| in cartesian coordinates.

Note: The operation βˆ‡ f \boldsymbol{\nabla}f results in a vector and involves an operation on a scalar function f f ; the equation is read as β€œthe gradient of f f ”. In contrast, the operation βˆ‡ β‹… U \boldsymbol{\nabla}\boldsymbol{\cdot} \mathbf{U} results in a scalar function and involves an operation on a vector function U \mathbf{U} . See also the caution in the notes on divergence.

Question: It is simple to compute a vector function U \mathbf{U} given a scalar function f f using βˆ‡ f \boldsymbol{\nabla}f . Can we reverse this process – that is, given a vector function U \mathbf{U} , can we find a scalar function f f ?

The answer is yes, provided that βˆ‡ Γ— U = 0 \boldsymbol{\nabla} \times \mathbf{U} = 0 . The proof of this is given in 2.3.1 of Griffiths; it requires the Fundamental Theorem of Gradients and Stoke’s theorem, both of which will be covered later in the semester. At this point, we will only cover the result, which is

f ( r ) = f ( a ) + ∫ a r U β‹… d l f(\mathbf{r}) = f(\mathbf{a}) + \int_\mathbf{a}^\mathbf{\mathbf{r}}\mathbf{U}\boldsymbol{\cdot} d\mathbf{l}

where the line integral can be taken over any path from a \mathbf{a} to r \mathbf{r} .

The statement f ( r ) f(\mathbf{r}) is short–hand for f ( x , y , z ) f(x,y,z) ; the justification is that the vector r = x x ^ + y y ^ + z z ^ \mathbf{r}=x\mathbf{\hat{x}} + y\mathbf{\hat{y}} +z\mathbf{\hat{z}} ends at the point in space ( x , y , z ) (x,y,z) . Vectors in limits of integration may be unfamiliar – in the integral above, the upper limit of r \mathbf{r} means that the line integrated over ends at ( x , y , z ) (x,y,z) and the lower limit a \mathbf{a} means the line integrated over starts at the point ( a x , a y , a z ) (a_x,a_y,a_z) .

In E&M, we use E = βˆ’ U \mathbf{E}=-\mathbf{U} and V V for f f .

In this notation, given V V , we can compute E \mathbf{E} using

E = βˆ’ βˆ‡ V \mathbf{E}=-\boldsymbol{\nabla}V

and given E \mathbf{E} , we can compute V V using

V ( r ) = V ( a ) βˆ’ ∫ a r E β‹… d l V(\mathbf{r}) = V(\mathbf{a}) - \int_\mathbf{a}^\mathbf{\mathbf{r}}\mathbf{E}\boldsymbol{\cdot} d\mathbf{l}

This last formula is equivalent to the formula that was used in the previous section if we define Ξ” V = V ( r ) βˆ’ V ( a ) \Delta V=V(\mathbf{r})-V(\mathbf{a}) .

Suppose V = k q / r V=kq/r .

  1. Compute E \mathbf{E} .

  2. Use this computed E \mathbf{E} and V ( r ) = V ( a ) βˆ’ ∫ a r E β‹… d l \displaystyle V(\mathbf{r}) = V(\mathbf{a}) - \int_\mathbf{a}^\mathbf{\mathbf{r}}\mathbf{E}\boldsymbol{\cdot} d\mathbf{l} to compute V V .

For the path, use a straight line between a = ( R x ^ + R y ^ ) / 2 \mathbf{a}=(R\mathbf{\hat{x}} + R\mathbf{\hat{y}})/\sqrt{2} to r = r ( x ^ + y ^ ) / 2 \mathbf{r}=r(\mathbf{\hat{x}} + \mathbf{\hat{y}})/\sqrt{2}

Answer:

1.

From Griffiths, for f f in cartesian coordinates,

βˆ‡ f ( x , y , z ) = βˆ‚ f βˆ‚ x x ^ + βˆ‚ f βˆ‚ y y ^ + βˆ‚ f βˆ‚ z z ^ \boldsymbol{\nabla}f(x,y,z)=\frac{\partial f}{\partial x}\mathbf{\hat{x}}+\frac{\partial f}{\partial y}\mathbf{\hat{y}}+\frac{\partial f}{\partial z}\mathbf{\hat{z}}

We could use this equation by re-writing V V as k q / x 2 + y 2 + z 2 kq/\sqrt{x^2+y^2+z^2} . Alternatively, we can use the formula for the gradient in spherical coordinates:

βˆ‡ f ( r , ΞΈ , Ο• ) = βˆ‚ f βˆ‚ r r ^ + 1 r βˆ‚ f βˆ‚ ΞΈ ΞΈ ^ + 1 r sin ⁑ ΞΈ βˆ‚ f βˆ‚ Ο• Ο• ^ \boldsymbol{\nabla} f(r,\theta,\phi) = {\partial f \over \partial r}\hat{\mathbf r}+ {1 \over r}{\partial f \over \partial \theta}\hat{\boldsymbol \theta}+ {1 \over r\sin\theta}{\partial f \over \partial \phi}\hat{\boldsymbol \phi}

Using this, we need to compute E = βˆ’ βˆ‡ V = βˆ’ ( βˆ‚ V βˆ‚ r r ^ + 1 r βˆ‚ V βˆ‚ ΞΈ ΞΈ ^ + 1 r sin ⁑ ΞΈ βˆ‚ V βˆ‚ Ο• Ο• ^ ) \mathbf{E}=-\boldsymbol{\nabla} V=-\left({\partial V \over \partial r}\hat{\mathbf r}+ {1 \over r}{\partial V \over \partial \theta}\hat{\boldsymbol \theta}+ {1 \over r\sin\theta}{\partial V \over \partial \phi}\hat{\boldsymbol \phi}\right)

The last two terms are zero because V V does not depend on ΞΈ \theta or Ο• \phi . This leaves

E = βˆ’ βˆ‚ ( k q r ) βˆ‚ r r ^ = k q r 2 r ^ \mathbf{E}=-{\partial (\frac{kq}{r}) \over \partial r}\hat{\mathbf r} = \frac{kq}{r^2}\hat{\mathbf r}

Given that this electric field is that of a point charge at the origin, we conclude that the given V V is also that for a point charge at the origin.

2.

We need to evaluate V ( r ) = V ( a ) βˆ’ ∫ a r E β‹… d l \displaystyle V(\mathbf{r}) = V(\mathbf{a}) - \int_\mathbf{a}^{\mathbf{r}}\mathbf{E}\boldsymbol{\cdot} d\mathbf{l}

The integral will be straight–forward to compute if we write d l d\mathbf{l} in spherical coordinates, which is d l = d r r ^ d\mathbf{l}=dr\hat{\mathbf r} along a radial line (See 1.4.1 of Griffiths).

V ( r ) = V ( a ) βˆ’ ∫ a r k q r 2 r ^ β‹… ( d r r ^ ) = V ( a ) βˆ’ ∫ a r k q r 2 d r = V ( a ) βˆ’ [ βˆ’ k q r ] a r = V ( a ) + k q r βˆ’ k q a \begin{aligned} V(\mathbf{r})=&V(\mathbf{a})- \int_a^{r}\frac{kq}{r^2}\hat{\mathbf r}\boldsymbol{\cdot} (dr\hat{\mathbf r})\\ =&V(\mathbf{a})-\int_a^{r}\frac{kq}{r^2}dr=V(\mathbf{a})-\left[-\frac{kq}{r}\right]_a^r\\ =&V(\mathbf{a})+\frac{kq}{r}-\frac{kq}{a} \end{aligned}

The first and last terms on the right–hand side are constants. As a result, we have found

V ( r ) = c o n s t + k q r \displaystyle V(\mathbf{r})=const + \frac{kq}{r}

which is equal to the V V that we started with only if c o n s t = 0 const=0 . This constant cannot be determined unless we are given V V at some reference point. That is, given E \mathbf{E} , we cannot uniquely compute V V unless we are given V V at some position in space.

Another way explaining this is to consider a similar problem: if F = d f / d x F=df/dx , show that ∫ a x F ( x β€² ) d x β€² \int_a^x F(x')dx' gives f f . If f = x 2 f=x^2 , then F = 2 x F=2x and ∫ a x F ( x β€² ) d x β€² = x 2 βˆ’ f ( a ) \int_a^x F(x') dx'= x^2 - f(a) . We can’t show that ∫ F ( x β€² ) d x β€² \int F(x')dx' gives f f unless we are told that the constant from integration, f ( a ) f(a) , is zero.

Although it does not make sense to say β€œ V = k q / r V=kq/r ” without also giving the potential at a reference point, we do it anyway. The convention is that if a potential at a reference point is not given, then the reference point is infinity and the reference potential is zero. That is, instead of stating β€œ V = k q / r V=kq/r with V ( r = ∞ ) = 0 V(r=\infty)=0 ”, we simply state β€œ V = k q / r V=kq/r ”.

Plot V ( x ) V(x) for Example 4.1 in the Gauss’s law notes. Assume V ( 0 ) = 0 V(0)=0 .

Answer

The electric field plot from the solution is shown below.

The potential will not change between βˆ’ t / 2 ≀ x ≀ t / 2 -t/2 \le x \le t/2 because the electric field is zero inside of a conductor.

To get V ( x ) V(x) for x > t / 2 x>t/2 , solve

V ( x ) = V ( t / 2 ) βˆ’ ∫ t / 2 x E x ( x β€² ) d x β€² \displaystyle V(x) = V(t/2) - \int_{t/2}^x E_x(x')dx'

Using V ( t / 2 ) = 0 V(t/2)=0 and E x = Οƒ / Ο΅ o E_x = \sigma/\epsilon_o gives

V ( x ) = βˆ’ ∫ t / 2 x Οƒ Ο΅ o d x β€² = βˆ’ Οƒ Ο΅ o ( x βˆ’ t 2 ) for  x > t / 2 \displaystyle V(x) = -\int_{t/2}^x \frac{\sigma}{\epsilon_o} dx'=-\frac{\sigma}{\epsilon_o}\left(x-\frac{t}{2}\right)\qquad\text{for } x\gt t/2

Check: V ( t / 2 ) V(t/2) should be zero and the potential should decrease as x x increases.

To get V ( x ) V(x) for x > t / 2 x>t/2 , solve

V ( x ) = V ( βˆ’ t / 2 ) βˆ’ ∫ βˆ’ t / 2 x E x ( x β€² ) d x β€² \displaystyle V(x) = V(-t/2) - \int_{-t/2}^x E_x(x')dx'

Using V ( βˆ’ t / 2 ) = 0 V(-t/2)=0 and E x = βˆ’ Οƒ / Ο΅ o E_x = -\sigma/\epsilon_o gives

V ( x ) = βˆ’ ∫ βˆ’ t / 2 x βˆ’ Οƒ Ο΅ o d x β€² = Οƒ Ο΅ o ( x + t 2 ) for  x < t / 2 \displaystyle V(x) = -\int_{-t/2}^x -\frac{\sigma}{\epsilon_o} dx'=\frac{\sigma}{\epsilon_o}\left(x+\frac{t}{2}\right)\qquad\text{for } x\lt t/2

Check: V ( βˆ’ t / 2 ) V(-t/2) should be zero and the potential should increase as x x increases.

It is quite easy to lose a negative sign when doing this computation. There are two ways to check your answer:

  1. V ( x ) V(x) should be continuous

  2. V ( x ) V(x) should decrease when you move in the direction of the electric field. Thus, I expect that as I move from x = t / 2 x=t/2 to larger x x , V ( x ) V(x) should decrease because the electric field is in the + x +x direction. As I move from large negative x x towards the slab, I expect the potential to increase because I am moving against the electric field. (It may help to add field lines to the drawing above.)

The electric field lines shown are for the field E = k q r ^ / r 2 \mathbf{E}= {kq\hat{\mathbf r}}/{r^2} . Compute V ( r ) V(\mathbf{r}) using V ( r ) = V ( a ) βˆ’ ∫ a b E β‹… d l V(\mathbf{r}) = V(\mathbf{a}) - \int_\mathbf{a}^\mathbf{\mathbf{b}}\mathbf{E}\boldsymbol{\cdot} d\mathbf{l} and assuming V ( r = ∞ ) = 0 V(r=\infty)=0 for

  1. Path 1

  2. Path 2

Show and justify all steps in your calculation.

Partial Answer:

We expect the answers to be the same because the line integral of E \mathbf{E} applies to arbitrary paths.

For a point charge at the origin, E = k q r ^ / r 2 \mathbf{E}=kq\hat{\mathbf r}/r^2 , the calculation of

V ( r ) = V ( a ) βˆ’ ∫ a r E β‹… d l V(\mathbf{r}) = V(\mathbf{a}) - \int_\mathbf{a}^\mathbf{\mathbf{r}}\mathbf{E}\boldsymbol{\cdot} d\mathbf{l}

was given in an example in the previous section and the result was

V ( r ) = c o n s t + k q r V(\mathbf{r}) = const + \frac{kq}{r}

By convention, for point charges at any location, we always assume that V ( ∞ ) = 0 V(\infty)=0 , so c o n s t const can be solved for using

V ( r = ∞ ) = 0 = c o n s t + k q ∞ β‡’ c o n s t = 0 V(r=\infty) = 0 = const + \frac{kq}{\infty}\quad \Rightarrow\quad const = 0

For a point charge not at the origin, the potential with respect to a coordinate system centered on the charge depends on the radial distance Τ‰ \char"0509 from the point charge to the point of interest:

V ( Τ‰ ) = k q Τ‰ V(\textbf{\char"0509}) = \frac{kq}{\char"0509}

where Τ‰ = r βˆ’ r β€² \textbf{\char"0509}=\mathbf{r}-\mathbf{r}' , r \mathbf{r} is a vector from the origin to the point of interest and r β€² \mathbf{r}' is a vector from the origin to the point charge. By convention, we usually omit the functional dependence in V V . Or, we write the functional dependence as V ( r ) V(\mathbf{r}) because r β€² \mathbf{r}' is usually fixed or given and we care about how V V varies relative to an origin that is not at the location of the charge. Thus, we usually write

V ( r ) = k q ∣ r βˆ’ r β€² ∣ \boxed{V(\mathbf{r}) = \frac{kq}{|\mathbf{r}-\mathbf{r}'|}}

Recall that the electric field due to a point charge at r β€² \mathbf{r}' is

E ( r ) = k q ∣ r βˆ’ r β€² ∣ 3 ∣ r βˆ’ r β€² ∣ 3 \mathbf{E}(\mathbf{r})=kq\frac{\phantom{|}\mathbf{r}-\mathbf{r}'\phantom{|^3}}{|\mathbf{r}-\mathbf{r}'|^3}

You have already shown that these two equations satisfy E = βˆ’ βˆ‡ V \mathbf{E}=-\boldsymbol{\nabla}V in HW #1, where you showed that βˆ‡ ( 1 ∣ r βˆ’ r β€² ∣ ) = βˆ’ ∣ r βˆ’ r β€² ∣ 3 ∣ r βˆ’ r β€² ∣ 3 \boldsymbol{\nabla}\left(\frac{1}{|\mathbf{r}-\mathbf{r}'|}\right)=\displaystyle -\frac{\phantom{|}\mathbf{r}-\mathbf{r}'\phantom{|^3}}{|\mathbf{r}-\mathbf{r}'|^3} .

A point q q is at ( x , y , z ) = ( R , R , R ) / 3 (x,y,z)=(R,R,R)/\sqrt{3} . Compute V ( x , y , z ) V(x,y,z) .

Answer

r = x x ^ + y y ^ + z z ^ \mathbf{r}=x\mathbf{\hat{x}} + y\mathbf{\hat{y}} + z\mathbf{\hat{z}}

r β€² = R x ^ + R y ^ + R z ^ \mathbf{r}'=R\mathbf{\hat{x}} + R\mathbf{\hat{y}} + R\mathbf{\hat{z}}

V ( r ) = k q Τ‰ = k q ∣ r βˆ’ r β€² ∣ = k q 1 ( x βˆ’ R ) 2 + ( y βˆ’ R ) 2 + ( z βˆ’ R ) 2 \displaystyle V(\mathbf{r}) = \frac{kq}{\char"0509}= \frac{kq}{|\mathbf{r}-\mathbf{r}'|}=kq\frac{1}{\sqrt{(x-R)^2+(y-R)^2+(z-R)^2}}

A way of checking this equation is to note that the potential is expected to become large as you approach the position of a charge. Plugging in ( x , y , z ) = ( R , R , R ) (x,y,z)=(R,R,R) makes the denominator zero.

A point q 1 q_1 charge is at ( x , y , z ) = ( b , 0 , 0 ) (x,y,z)=(b,0,0) . A point charge q 2 q_2 is at ( x , y , z ) = ( βˆ’ b , 0 , 0 ) (x,y,z)=(-b,0,0) . Write the equation for V V as the sum of V 1 + V 2 V_1+V_2 for each charge and then use E = βˆ’ βˆ‡ V \mathbf{E}=-\boldsymbol{\nabla}V to compute E \mathbf{E} .

Previously, differences in electric potential energy, Ξ” P E \Delta PE , and electric potential, Ξ” V \Delta V , were considered. Only differences in P E PE and V V are meaningful. However, in E&M, we often discuss P E PE and V V ; in this case, these quantities are relative to the respective quantities for a charge at infinity, in which case P E PE and V V are zero. That is, instead of discussing Ξ” P E \Delta PE in the equation Ξ” P E = P E ( r ) βˆ’ P E ( r = ∞ ) \Delta PE = PE(r) - PE(r={\infty}) , we discuss P E ( r ) PE(r) , which is equal to Ξ” P E \Delta PE because P E ( ∞ ) PE({\infty}) was chosen to be zero. A similar statement applies to V V .

Using this convention, the electric potential energy of a charge q 0 q_0 at a position r = x x ^ + y y ^ + z z ^ \mathbf{r}=x\mathbf{\hat{x}} + y\mathbf{\hat{y}} + z\mathbf{\hat{z}} that is a distance of Τ‰ 1 \char"0509_1 from a charge q 1 q_1 is

P E = k q 0 q 1 Τ‰ 01 PE=k\frac{q_0q_1}{\char"0509_{01}}

In this formula, if the charges have opposite signs then P E PE is negative; if they have the same sign then P E PE is positive. Note that there is a sign associated with the potential energy but the direction of the vector that connects the charges does not matter; the equation for P E PE only involves the values of the charges and the magnitude of the separation distance Τ‰ 01 \char"0509_{01} between them.

Consider next the potential energy of charge q 0 q_0 when it is a distance r 1 r_1 from charge q 1 q_1 and a distance r 2 r_2 from charge q 2 q_2 . Work is required to move q 0 q_0 in the field due to q 1 q_1 and also the field due to q 2 q_2 . The total potential energy of q 0 q_0 is the sum of these works:

P E = k q 0 q 1 Τ‰ 01 + k q 0 q 2 Τ‰ 02 PE=k\frac{q_0q_1}{\char"0509_{01}}+k\frac{q_0q_2}{\char"0509_{02}}

More generally, if there is a group of N N charges, the potential energy of charge q 0 q_0 is

P E = k q 0 βˆ‘ i = 1 N q i Τ‰ 0 i PE=k q_0 \sum_{i=1}^N {\frac{q_i}{\char"0509_{0i}}}

Using V = P E / q o V=PE/q_o , the electric potential at a point in space r \mathbf{r} due to a group of N N charges is the sum of the potentials due to each of the charges at r \mathbf{r}

V ( r ) = k βˆ‘ i = 1 N q i Τ‰ i V(\mathbf{r})=k \sum_{i=1}^N {\frac{q_i}{\char"0509_i}}

In this equation, we have dropped the subscript 0 0 from the positions because it is implied that all of the distances are relative to the location r \mathbf{r} where we want to compute V V .

1. What is the potential energy of the charge q 0 q_0 in the diagram shown?

Answer: P E = k q o q 1 Τ‰ 01 + k q o q 2 Τ‰ 02 + k q o q 3 Τ‰ 03 PE = \frac{kq_oq_1}{\char"0509_{01}}+\frac{kq_oq_2}{\char"0509_{02}}+\frac{kq_oq_3}{\char"0509_{03}}

This represents the amount of energy it would take to move charge q o q_o from infinity to its position on the diagram.

2. What is the potential at the position of q 0 q_0 if that charge were to be removed (i.e., the potential due to charges q 1 q_1 , q 2 q_2 , and q 3 q_3 )?

Answer

Using P E = V / q o PE=V/q_o , V = k q 1 Τ‰ 1 + k q 2 Τ‰ 2 + k q 3 Τ‰ 3 \displaystyle V = \frac{kq_1}{\char"0509_1}+\frac{kq_2}{\char"0509_2}+\frac{kq_3}{\char"0509_3}

That is, the potential at a given location is found from potential energy of a charge at that location by dividing by the charge’s potential energy by the value of the charge.

3. Can you find the potential energy at the position of q 0 q_0 if that charge were to be removed? Why or why not?

Answer: No. It does not make sense to ask what the potential energy is at a point in space. Only physical objects (e.g., masses, charges) have potential energy.

4. Explain the difference between potential and potential energy.

Answer: A potential is a value associated with a location in space, and an electric potential is created by charges at all locations in space.

Potential energy is the energy associated with an object at a given location in space. The electric potential energy of a charge is the energy required to move it from a large distance away from all other charges to a given location in space. The electric potential energy of a charge Q Q at a point in space is related to the electric potential at that point in space by P E = Q V PE=QV .

In the previous section, the electric potential V V . The quantity q V ( r ) qV(\mathbf{r}) corresponds to the change in potential energy ( Ξ” P E \Delta PE ) of q q if it is moved from a reference location with V = 0 V=0 to the point r \mathbf{r} . This change in potential energy is also equal to the work required to move q q to r \mathbf{r} .

When there are only two charges q 1 q_1 and q 2 q_2 separated by a distance r r , the work required to move them into position is k q 1 q 2 / r kq_1q_2/r , which is V 1 q 2 V_1q_2 and also q 1 V 2 q_1V_2 .

Another consideration is the energy required to create a charge distribution. This energy is denoted as W W in Griffiths. An example of a charge distribution is shown in the following figure.

  • q V ( r ) qV(\mathbf{r}) is the work required to move q q to r \mathbf{r} against the electric field due to all of the other charges. The other charges have been β€œpreassembled”

  • W W is the work required to assemble a charge distribution.

To compute W W , for the following charge distribution, we need to compute the energy required to move each charge from infinity to their final position.

To compute the W W , we start by moving the left charge q 1 q_1 from infinity to its position at x = βˆ’ b x=-b . There is no electric field, so no work is required.

To move q 2 q_2 into place, we must do work against the elecric field created by q 1 q_1 . This work is V 1 q 2 = k q 1 q 2 / b V_1q_2 = kq_1q_2/b .

To move q 3 q_3 into place, we must do work against the electric field created by q 1 q_1 and q 2 q_2 . This work is V 1 q 3 = k q 1 q 3 / b V_1q_3=kq_1q_3/b + V 2 q 3 = k q 2 q 3 / 2 b V_2q_3=kq_2q_3/2b . Thus,

W = k q 1 q 2 b + k q 1 q 3 b + k q 2 q 3 2 b W=k\frac{q_1q_2}{b} + k\frac{q_1q_3}{b} + k\frac{q_2q_3}{2b}

This can be generalized using the notation of Griffiths, where Τ‰ i j {\char"0509}_{ij} is the distance between q i q_i and q j q_j .

W = k q 1 q 2 Τ‰ 12 + k q 1 q 3 Τ‰ 13 + k q 2 q 3 Τ‰ 23 W=k\frac{q_1q_2}{{\char"0509}_{12}} + k\frac{q_1q_3}{{\char"0509}_{13}} + k\frac{q_2q_3}{{\char"0509}_{23}}

where r 1 = βˆ’ b x ^ \mathbf{r}_1=-b\mathbf{\hat{x}} , r 2 = 0 \mathbf{r}_2=0 , and r 3 = b x ^ \mathbf{r}_3=b\mathbf{\hat{x}} and Τ‰ 12 = ∣ r 1 βˆ’ r 2 ∣ {\char"0509}_{12}=|\mathbf{r}_1-\mathbf{r}_2| , Τ‰ 13 = ∣ r 1 βˆ’ r 3 ∣ {\char"0509}_{13}=|\mathbf{r}_1-\mathbf{r}_3| , and Τ‰ 23 = ∣ r 2 βˆ’ r 3 ∣ {\char"0509}_{23}=|\mathbf{r}_2-\mathbf{r}_3|

For the following charge distribution, compute

  1. the electric potential at the origin,

  2. the electric potential at any position x , y x,y , and

  3. the work required to assemble the charge distribution.

Answer

1. A common error was having a term in V V that was k q 1 / ( βˆ’ b ) kq_1/(-b) . The denominator of potential is a length, so it must be positive. Also, many student wrote an answer for part 2. that was correct but when x = y = 0 x=y=0 was plugged in, they did not get the same equation they wrote for part 1.

1. and 2.

V ( r ) = k βˆ‘ i = 1 3 q i Τ‰ i V(\mathbf{r})=k \sum_{i=1}^3 {\frac{q_i}{\char"0509_i}}

Τ‰ 1 = ∣ r βˆ’ r 1 β€² ∣ = ∣ x x ^ + y y ^ βˆ’ ( βˆ’ b ) x ^ ∣ = ( x + b ) 2 + y 2 \char"0509_1=|\mathbf{r}-\mathbf{r}_1'|=|x\mathbf{\hat{x}}+y\mathbf{\hat{y}}-(-b)\mathbf{\hat{x}}|=\sqrt{(x+b)^2+y^2}

Τ‰ 2 = ∣ r βˆ’ r 2 β€² ∣ = ∣ x x ^ + y y ^ βˆ’ b x ^ ∣ = ( x βˆ’ b ) 2 + y 2 \char"0509_2=|\mathbf{r}-\mathbf{r}_2'|=|x\mathbf{\hat{x}}+y\mathbf{\hat{y}}-b\mathbf{\hat{x}}|=\sqrt{(x-b)^2+y^2}

Τ‰ 3 = ∣ r βˆ’ r 3 β€² ∣ = ∣ x x ^ + y y ^ βˆ’ b y ^ ∣ = x 2 + ( y βˆ’ b ) 2 \char"0509_3=|\mathbf{r}-\mathbf{r}_3'|=|x\mathbf{\hat{x}}+y\mathbf{\hat{y}}-b\mathbf{\hat{y}}|=\sqrt{x^2+(y-b)^2}

So the answer to 2. is

V ( x , y ) = k ( q 1 ( x + b ) 2 + y 2 + q 2 ( x βˆ’ b ) 2 + y 2 + q 3 x 2 + ( y βˆ’ b ) 2 ) \displaystyle V(x,y)=k\left(\frac{q_1}{\sqrt{(x+b)^2+y^2}}+\frac{q_2}{\sqrt{(x-b)^2+y^2}}+\frac{q_3}{\sqrt{x^2+(y-b)^2}}\right)

Plugging in x = y = 0 x=y=0 gives the answer to 1.

V ( x , y ) = k ( q 1 b + q 2 b + q 3 b ) \displaystyle V(x,y)=k\left(\frac{q_1}{b}+\frac{q_2}{b}+\frac{q_3}{b}\right)

3.

W = k q 1 q 2 2 b + k q 1 q 3 2 b + k q 2 q 3 2 b \displaystyle W=\frac{kq_1q_2}{\sqrt{2}b}+\frac{kq_1q_3}{2b} + \frac{kq_2q_3}{\sqrt{2}b}