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Part A – Angular Speed
| Step | Derivation/Formula | Reasoning |
|---|---|---|
| 1 | \[T\cos(\theta)=mg\] | The vertical component of the tension \(T\) balances the gravitational force \(mg\) on the ball. |
| 2 | \[T\sin(\theta)=m\omega^2r\] | The horizontal component of \(T\) provides the centripetal force (\(m\omega^2r\)) needed for circular motion. |
| 3 | \[\frac{T\sin(\theta)}{T\cos(\theta)}=\frac{m\omega^2r}{mg}\] | Dividing the horizontal equation by the vertical one eliminates \(T\) to relate \(\omega\) and \(\theta\). |
| 4 | \[\tan(\theta)=\frac{\omega^2r}{g}\] | This simplifies the relationship between the angle \(\theta\) and the angular speed \(\omega\). |
| 5 | \[\omega^2=\frac{g\tan(\theta)}{r}\] | Solving for \(\omega^2\) in terms of \(\tan(\theta)\), \(r\), and \(g\). |
| 6 | \[\sin(\theta)=\frac{r}{\ell}\quad \text{and}\quad \cos(\theta)=\sqrt{1-\frac{r^2}{\ell^2}}=\frac{\sqrt{\ell^2-r^2}}{\ell}\] | Using the geometry of the conical pendulum, where the horizontal radius \(r\) relates to the string length \(\ell\) and angle \(\theta\). |
| 7 | \[\tan(\theta)=\frac{\sin(\theta)}{\cos(\theta)}=\frac{r}{\sqrt{\ell^2-r^2}}\] | Expressing \(\tan(\theta)\) in terms of the given variables \(r\) and \(\ell\). |
| 8 | \[\omega^2=\frac{g}{r}\cdot\frac{r}{\sqrt{\ell^2-r^2}}=\frac{g}{\sqrt{\ell^2-r^2}}\] | Substituting the expression for \(\tan(\theta)\) into the equation for \(\omega^2\) simplifies the result. |
| 9 | \[\boxed{\omega=\sqrt{\frac{g}{\sqrt{\ell^2-r^2}}}}\] | Taking the square root yields the final expression for the angular speed \(\omega\) in terms of \(\ell\), \(r\), and \(g\). |
Part B – Tension
| Step | Derivation/Formula | Reasoning |
|---|---|---|
| 1 | \[T\cos(\theta)=mg\] | The vertical component of the tension balances the weight of the ball. |
| 2 | \[T=\frac{mg}{\cos(\theta)}\] | Solving for the tension \(T\) from the vertical equilibrium equation. |
| 3 | \[\cos(\theta)=\frac{\sqrt{\ell^2-r^2}}{\ell}\] | Expressing \(\cos(\theta)\) in terms of the string length \(\ell\) and the horizontal radius \(r\) using geometry. |
| 4 | \[T=\frac{mg}{\frac{\sqrt{\ell^2-r^2}}{\ell}}=\frac{mg\ell}{\sqrt{\ell^2-r^2}}\] | Substituting \(\cos(\theta)\) into the equation for \(T\) and simplifying. |
| 5 | \[\boxed{T=\frac{mg\ell}{\sqrt{\ell^2-r^2}}}\] | This is the final expression for the tension \(T\) in the string in terms of \(L\) (\(\ell\)), \(m\), \(r\), and \(g\). |
Just ask: "Help me solve this problem."
A \( 1.5 \) \( \text{kg} \) block is pushed to the right with just enough force to get it to move. The block is pushed for five seconds with this constant force, then the force is released and the block slides to a stop. If the coefficient of kinetic friction is \( 0.300 \) and the coefficient of static friction is \( 0.400 \), calculate the amount of time that passes from when the force is applied to when the block stops.
What is a man’s apparent weight at the equator if his weight is \(500 \, \text{N}\)? The Earth’s radius is \(6.37 \times 10^{6} \, \text{m}\).
A space probe far from the Earth is travelling at \( 14.8 \) \( \text{km s}^{-1} \). It has mass \( 1\,312 \) \( \text{kg} \). The probe fires its rockets to give a constant thrust of \( 156 \) \( \text{kN} \) for \( 220. \) \( \text{s} \). It accelerates in the same direction as its initial velocity. In this time it burns \( 150. \) \( \text{kg} \) of fuel.
Calculate the final speed of the space probe in \( \text{km s}^{-1} \).
During lunch, Alex and Jordan argue about inertia. Alex says if she spins a basketball faster, it will have greater inertia. Jordan argues that inertia only depends on the ball’s mass, not its speed. Who is correct?
A \(1 \, \text{kg}\) mass and an unknown mass \(M\) hang on opposite sides of a pulley suspended from the ceiling. When the masses are released, \(M\) accelerates downward at \(5 \, \text{m/s}^2\). Find the value of \(M\).
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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] |
General Metric Conversion Chart
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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