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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 roller coaster ride at an amusement park lifts a car of mass \( 700 \, \text{kg} \) to point \( A \) at a height of \( 90 \, \text{m} \) above the lowest point on the track, as shown above. The car starts from rest at \( A \), rolls with negligible friction down the incline and follows the track around a loop of radius \( 20 \, \text{m} \). Point \( B \), the highest point on the loop, is at a height of \( 50 \, \text{m} \) above the lowest point on the track.
A [katex] 2.2 \times 10^{21} \, \text{kg}[/katex] moon orbits a distant planet in a circular orbit of radius [katex] 1.5 \times 10^8 \, \text{m}[/katex]. It experiences a [katex] 1.1 \times 10^{19} \, \text{N}[/katex] gravitational pull from the planet. What is the moon’s orbital period in earth days?
Two blocks made of different materials, connected by a thin cord, slide down a plane ramp inclined at an angle \( \theta = 32^\circ \) above the horizontal. If the coefficients of friction are \( \mu_A = 0.2 \) and \( \mu_B = 0.3 \) and if \( m_A = m_B = 5.0 \) \( \text{kg} \), determine:
An Olympic bobsled team goes through a horizontal curve at a speed of \( 120 \) \( \text{km/hr} \). If the radius of curvature is \( 10.0 \) \( \text{m} \), what is the apparent weight the crew experiences—express in terms of \( mg \)?
A block of mass \( m \), acted on by a force \( F \) directed horizontally, slides up an inclined plane that makes an angle \( \theta \) with the horizontal. The coefficient of sliding friction between the block and the plane is \( \mu \).
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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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