| Step | Derivation / Formula | Reasoning |
|---|---|---|
| 1 | \[T\cos\theta = mg\] | Vertical acceleration is zero, so the vertical component of the tension balances the weight. |
| 2 | \[T = \frac{mg}{\cos\theta}\] | Solve the equilibrium equation for the tension \(T\). |
| 3 | \[\sin\theta = \frac{R}{L},\qquad \cos\theta = \sqrt{1-\frac{R^{2}}{L^{2}}}\] | Geometry of the conical pendulum: the string makes an angle \(\theta\) with the vertical, so \(R = L\sin\theta\). |
| 4 | \[\boxed{\displaystyle T = \frac{mg}{\sqrt{1-\frac{R^{2}}{L^{2}}}}}\] | Substitute the expression for \(\cos\theta\) from Step 3 into Step 2. |
| Step | Derivation / Formula | Reasoning |
|---|---|---|
| 1 | \[T\sin\theta = m\frac{v^{2}}{R}\] | The horizontal component of the tension provides the required centripetal force. |
| 2 | \[v^{2} = \frac{T R\sin\theta}{m}\] | Solve Step 1 for \(v^{2}\). |
| 3 | \[v^{2} = \frac{(mg/\cos\theta)\,R\sin\theta}{m}=gR\tan\theta\] | Substitute \(T=mg/\cos\theta\); the mass \(m\) cancels. |
| 4 | \[v = \sqrt{gR\tan\theta}\] | Take the square root to find the speed. |
| 5 | \[P = \frac{2\pi R}{v}\] | The period is the circumference divided by the speed. |
| 6 | \[P = \frac{2\pi R}{\sqrt{gR\tan\theta}} = 2\pi \sqrt{\frac{R}{g\tan\theta}}\] | Insert \(v\) from Step 4 and simplify correctly (retain one factor of \(R\) under the square root). |
| 7 | \[\tan\theta = \frac{\sin\theta}{\cos\theta}=\frac{R/L}{\sqrt{1-\frac{R^{2}}{L^{2}}}}=\frac{R}{\sqrt{L^{2}-R^{2}}}\] | Express \(\tan\theta\) using the geometry from Part (a). |
| 8 | \[P = 2\pi \sqrt{\frac{R}{g\left(\frac{R}{\sqrt{L^{2}-R^{2}}}\right)}} = 2\pi \sqrt{\frac{\sqrt{L^{2}-R^{2}}}{g}}\] | Substitute \(\tan\theta\) from Step 7 into Step 6 and cancel \(R\). |
| 9 | \[P = 2\pi \sqrt{\frac{L\cos\theta}{g}}\] | Since \(\sqrt{L^{2}-R^{2}} = L\cos\theta\), this is an equivalent compact form. |
| 10 | \[\boxed{\displaystyle P = 2\pi \sqrt{\frac{L\sqrt{1-\frac{R^{2}}{L^{2}}}}{g}}}\] | Express the period solely in terms of \(L\), \(R\), and \(g\). |
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Friction provides the force needed for a car to travel around a flat, circular race track. Answer the following:
A \(2.2 \times 10^{21} \, \text{kg}\) moon orbits a distant planet in a circular orbit of radius \(1.5 \times 10^8 \, \text{m}\). It experiences a \(1.1 \times 10^{19} \, \text{N}\) gravitational pull from the planet. What is the moon’s orbital period in Earth days?
A car is going over the top of a hill whose curvature approximates a circle of radius \( 350 \) \( \text{m} \). At what velocity will the occupants of the car appear to weigh \( 10\% \) less than their normal weight?
Which of the following best explains why astronauts experience weightlessness while orbiting the earth?
The Moon does not crash into the Earth because:
Why do pilots sometimes black out while pulling out at the bottom of a dive?
A group of astronauts in a spaceship are attempting to land on Mars. As they approach the planet, they begin to plan their descent to the surface.
A centripetal force of \( 5.0 \) newtons is applied to a rubber stopper moving at a constant speed in a horizontal circle. If the same force is applied, but the radius is made smaller, what happens to the speed, \( v \), and the frequency, \( f \), of the stopper?
Are astronauts really “weightless” while in orbit?
A planet of constant mass orbits the sun in an elliptical orbit. Neglecting any friction effects, what happens to the planet’s rotational kinetic energy about the sun’s center?
\(T = \frac{mg}{\sqrt{1 – \frac{R^{2}}{L^{2}}}}\)
\(P = 2\pi \sqrt{\frac{L\sqrt{1 – \frac{R^{2}}{L^{2}}}}{g}}\)
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| Kinematics | Forces |
|---|---|
| \(\Delta x = v_i t + \frac{1}{2} at^2\) | \(F = ma\) |
| \(v = v_i + at\) | \(F_g = \frac{G m_1 m_2}{r^2}\) |
| \(v^2 = v_i^2 + 2a \Delta x\) | \(f = \mu N\) |
| \(\Delta x = \frac{v_i + v}{2} t\) | \(F_s =-kx\) |
| \(v^2 = v_f^2 \,-\, 2a \Delta x\) |
| Circular Motion | Energy |
|---|---|
| \(F_c = \frac{mv^2}{r}\) | \(KE = \frac{1}{2} mv^2\) |
| \(a_c = \frac{v^2}{r}\) | \(PE = mgh\) |
| \(T = 2\pi \sqrt{\frac{r}{g}}\) | \(KE_i + PE_i = KE_f + PE_f\) |
| \(W = Fd \cos\theta\) |
| Momentum | Torque 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 Motion | Fluids |
|---|---|
| \(F = -kx\) | \(P = \frac{F}{A}\) |
| \(T = 2\pi \sqrt{\frac{l}{g}}\) | \(P_{\text{total}} = P_{\text{atm}} + \rho gh\) |
| \(T = 2\pi \sqrt{\frac{m}{k}}\) | \(Q = Av\) |
| \(x(t) = A \cos(\omega t + \phi)\) | \(F_b = \rho V g\) |
| \(a = -\omega^2 x\) | \(A_1v_1 = A_2v_2\) |
| Constant | Description |
|---|---|
| [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 |
| Variable | SI 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] |
| Variable | Derived 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.
Start with the given measurement: [katex]\text{5 km}[/katex]
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]
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]
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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