AP Physics

Unit 1 - Vectors and Kinematics

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Step Reasoning
Identify Ampère’s law as the tool connecting the magnetic field along a closed circular path to the enclosed current.
\[ \oint \vec{B} \cdot d\vec{\ell} = \mu_0 I_{\text{enc}} \]
The question asks for the magnetic field magnitude \(B(r)\) inside a cylindrically symmetric current distribution.
Evaluate the line integral around a concentric circular path of radius \(r < R\).
\[ \oint \vec{B} \cdot d\vec{\ell} = B(r) \cdot 2\pi r \]
Cylindrical symmetry implies that the magnetic field is tangential and uniform in magnitude along the path of radius \(r\).
Set up and integrate the enclosed current \(I_{\text{enc}}(r)\) using thin cylindrical shells of area \(dA = 2\pi r’ \, dr’\).
\[ \begin{align*} I_{\text{enc}}(r) &= \int_0^r J(r’) \, dA = \int_0^r J_0 \left(1 – \dfrac{r’}{R}\right) (2\pi r’) \, dr’ \\ &= 2\pi J_0 \int_0^r \left(r’ – \dfrac{r’^2}{R}\right) dr’ \\ &= 2\pi J_0 \left[ \dfrac{r^2}{2} – \dfrac{r^3}{3R} \right] \end{align*} \]
Because current density depends on radial position \(r’\), total enclosed current requires integrating \(J(r’) \, dA\) from \(r’ = 0\) to \(r’ = r\).
Substitute \(I_{\text{enc}}(r)\) back into Ampère’s law and solve for \(B(r)\).
\[ \begin{align*} B(r) \cdot 2\pi r &= \mu_0 \cdot 2\pi J_0 \left( \dfrac{r^2}{2} – \dfrac{r^3}{3R} \right) \\ B(r) &= \mu_0 J_0 r \left( \dfrac{1}{2} – \dfrac{r}{3R} \right) = \dfrac{\mu_0 J_0 r}{2}\left(1 – \dfrac{2r}{3R}\right) \end{align*} \]
Equating the line integral from Step 2 to \(\mu_0 I_{\text{enc}}(r)\) allows solving directly for the field magnitude.

Why each choice is correct or incorrect:

(A) Incorrectly assumes that the enclosed current is given by multiplying the local current density at radius \(r\) by the total cross-sectional area, \(I_{\text{enc}} = J(r) \pi r^2\), instead of integrating \(J(r’) \, dA\).

(B) Omits the factor of \(r’\) in the differential area element by incorrectly using \(dA = 2\pi \, dr’\) rather than \(dA = 2\pi r’ \, dr’\).

(C) Evaluates \(\int_0^r r’ \, dr’\) incorrectly as \(r^2\) rather than \(\dfrac{r^2}{2}\), dropping the factor of \(\dfrac{1}{2}\) during integration.

(D) This is the correct answer.

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KinematicsForces
\(\Delta x = v_i t + \frac{1}{2} at^2\)\(F = ma\)
\(v = v_i + at\)\(F_g = \frac{G m_1 m_2}{r^2}\)
\(v^2 = v_i^2 + 2a \Delta x\)\(f = \mu N\)
\(\Delta x = \frac{v_i + v}{2} t\)\(F_s =-kx\)
\(v^2 = v_f^2 \,-\, 2a \Delta x\) 
Circular MotionEnergy
\(F_c = \frac{mv^2}{r}\)\(KE = \frac{1}{2} mv^2\)
\(a_c = \frac{v^2}{r}\)\(PE = mgh\)
\(T = 2\pi \sqrt{\frac{r}{g}}\)\(KE_i + PE_i = KE_f + PE_f\)
 \(W = Fd \cos\theta\)
MomentumTorque and Rotations
\(p = mv\)\(\tau = r \cdot F \cdot \sin(\theta)\)
\(J = \Delta p\)\(I = \sum mr^2\)
\(p_i = p_f\)\(L = I \cdot \omega\)
Simple Harmonic MotionFluids
\(F = -kx\)\(P = \frac{F}{A}\)
\(T = 2\pi \sqrt{\frac{l}{g}}\)\(P_{\text{total}} = P_{\text{atm}} + \rho gh\)
\(T = 2\pi \sqrt{\frac{m}{k}}\)\(Q = Av\)
\(x(t) = A \cos(\omega t + \phi)\)\(F_b = \rho V g\)
\(a = -\omega^2 x\)\(A_1v_1 = A_2v_2\)
ConstantDescription
[katex]g[/katex]Acceleration due to gravity, typically [katex]9.8 , \text{m/s}^2[/katex] on Earth’s surface
[katex]G[/katex]Universal Gravitational Constant, [katex]6.674 \times 10^{-11} , \text{N} \cdot \text{m}^2/\text{kg}^2[/katex]
[katex]\mu_k[/katex] and [katex]\mu_s[/katex]Coefficients of kinetic ([katex]\mu_k[/katex]) and static ([katex]\mu_s[/katex]) friction, dimensionless. Static friction ([katex]\mu_s[/katex]) is usually greater than kinetic friction ([katex]\mu_k[/katex]) as it resists the start of motion.
[katex]k[/katex]Spring constant, in [katex]\text{N/m}[/katex]
[katex] M_E = 5.972 \times 10^{24} , \text{kg} [/katex]Mass of the Earth
[katex] M_M = 7.348 \times 10^{22} , \text{kg} [/katex]Mass of the Moon
[katex] M_M = 1.989 \times 10^{30} , \text{kg} [/katex]Mass of the Sun
VariableSI Unit
[katex]s[/katex] (Displacement)[katex]\text{meters (m)}[/katex]
[katex]v[/katex] (Velocity)[katex]\text{meters per second (m/s)}[/katex]
[katex]a[/katex] (Acceleration)[katex]\text{meters per second squared (m/s}^2\text{)}[/katex]
[katex]t[/katex] (Time)[katex]\text{seconds (s)}[/katex]
[katex]m[/katex] (Mass)[katex]\text{kilograms (kg)}[/katex]
VariableDerived SI Unit
[katex]F[/katex] (Force)[katex]\text{newtons (N)}[/katex]
[katex]E[/katex], [katex]PE[/katex], [katex]KE[/katex] (Energy, Potential Energy, Kinetic Energy)[katex]\text{joules (J)}[/katex]
[katex]P[/katex] (Power)[katex]\text{watts (W)}[/katex]
[katex]p[/katex] (Momentum)[katex]\text{kilogram meters per second (kgm/s)}[/katex]
[katex]\omega[/katex] (Angular Velocity)[katex]\text{radians per second (rad/s)}[/katex]
[katex]\tau[/katex] (Torque)[katex]\text{newton meters (Nm)}[/katex]
[katex]I[/katex] (Moment of Inertia)[katex]\text{kilogram meter squared (kgm}^2\text{)}[/katex]
[katex]f[/katex] (Frequency)[katex]\text{hertz (Hz)}[/katex]

Metric Prefixes

Example of using unit analysis: Convert 5 kilometers to millimeters. 

  1. Start with the given measurement: [katex]\text{5 km}[/katex]

  2. Use the conversion factors for kilometers to meters and meters to millimeters: [katex]\text{5 km} \times \frac{10^3 \, \text{m}}{1 \, \text{km}} \times \frac{10^3 \, \text{mm}}{1 \, \text{m}}[/katex]

  3. Perform the multiplication: [katex]\text{5 km} \times \frac{10^3 \, \text{m}}{1 \, \text{km}} \times \frac{10^3 \, \text{mm}}{1 \, \text{m}} = 5 \times 10^3 \times 10^3 \, \text{mm}[/katex]

  4. Simplify to get the final answer: [katex]\boxed{5 \times 10^6 \, \text{mm}}[/katex]

Prefix

Symbol

Power of Ten

Equivalent

Pico-

p

[katex]10^{-12}[/katex]

Nano-

n

[katex]10^{-9}[/katex]

Micro-

µ

[katex]10^{-6}[/katex]

Milli-

m

[katex]10^{-3}[/katex]

Centi-

c

[katex]10^{-2}[/katex]

Deci-

d

[katex]10^{-1}[/katex]

(Base unit)

[katex]10^{0}[/katex]

Deca- or Deka-

da

[katex]10^{1}[/katex]

Hecto-

h

[katex]10^{2}[/katex]

Kilo-

k

[katex]10^{3}[/katex]

Mega-

M

[katex]10^{6}[/katex]

Giga-

G

[katex]10^{9}[/katex]

Tera-

T

[katex]10^{12}[/katex]

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