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| Step | Derivation / Formula | Reasoning |
|---|---|---|
| General set-up | \(\begin{aligned} \text{Let}&:\;T_y&=T\sin\theta \,\;(\text{vertical component of tension})\\ H_y&=\text{vertical component of wall force we seek}\\ a&=\text{block position ( }a=L\text{ or }L/2)\\ b&=\text{cable position ( }b=L\text{ or }L/2)\;. \end{aligned}\) | All four arrangements differ only in the values of a and b. The beam’s own weight \(Mg\) acts at \(L/2\). Horizontal components are irrelevant for the vertical reaction. |
| Static equilibrium conditions | Torque about wall hinge: \(T_y\,b = Mg\,\frac{L}{2}+Mg\,a\) Vertical forces: \(H_y + T_y -2Mg = 0\Rightarrow H_y = 2Mg – T_y\) |
Taking torques about the hinge eliminates the unknown horizontal wall force. The horizontal component of tension passes through the hinge and produces no torque, so only \(T_y\) appears. |
| (A) Cable at \(L\), Block at \(L\) | \(\begin{aligned} T_y &= Mg\,\frac{\dfrac{L}{2}+L}{L}=1.5\,Mg\\ H_y &= 2Mg-1.5Mg = 0.5\,Mg \end{aligned}\) | The upward lift supplied by the cable is \(1.5Mg\); the wall therefore needs to supply only \(0.5Mg\) upward. |
| (B) Cable at \(\tfrac{L}{2}\), Block at \(L\) | \(\begin{aligned} T_y &= Mg\,\frac{\dfrac{L}{2}+L}{\tfrac{L}{2}} = 3\,Mg\\ H_y &= 2Mg-3Mg = -1\,Mg\quad\Rightarrow\;|H_y| = 1\,Mg \end{aligned}\) | The cable lifts more than the total weight, so the wall must push downward with magnitude \(Mg\). |
| (C) Cable at \(L\), Block at \(\tfrac{L}{2}\) | \(\begin{aligned} T_y &= Mg\,\frac{\dfrac{L}{2}+\tfrac{L}{2}}{L}=1\,Mg\\ H_y &= 2Mg-1Mg = 1\,Mg \end{aligned}\) | With the block moved inward the cable lifts less, so the wall must supply \(Mg\) upward. |
| (D) Cable at \(\tfrac{L}{2}\), Block at \(\tfrac{L}{2}\) | \(\begin{aligned} T_y &= Mg\,\frac{\dfrac{L}{2}+\tfrac{L}{2}}{\tfrac{L}{2}} = 2\,Mg\\ H_y &= 2Mg-2Mg = 0 \end{aligned}\) | The cable’s upward force exactly balances the two weights, leaving the wall with no vertical reaction. |
| Comparison | \(|H_y|_{(A)} = 0.5Mg,\; |H_y|_{(B)} = Mg,\; |H_y|_{(C)} = Mg,\; |H_y|_{(D)} = 0\) | The smallest magnitude of the wall’s vertical force is zero, obtained in option (D). |
Just ask: "Help me solve this problem."
A solid ball of mass \( M \) and radius \( R \) has rotational inertia \( \frac{2}{5} M R^{2} \) about its center. It rolls without slipping along a level surface at speed \( v \) just before it begins rolling up an inclined plane. Which of the following expressions correctly represents the maximum vertical height the solid ball can ascend to when it rolls up the incline without slipping?
Which of the following must be true for an object at translational equilibrium?
A \( 4 \)-\( \text{kg} \) ball and a \( 1 \)-\( \text{kg} \) ball are positioned a distance \( L \) apart on a bar of negligible mass. How far from the \( 4 \)-\( \text{kg} \) mass should the fulcrum be placed to balance the bar?
A rotating, rigid body makes 10 complete revolutions in 10 seconds. What is its average angular velocity?
The driver of a car traveling at \( 30.0 \) \( \text{m/s} \) applies the brakes and undergoes a constant negative acceleration of \( 2.00 \) \( \text{m/s}^2 \). How many revolutions does each tire make before the car comes to a stop, assuming that the car does not skid and that the tires have radii of \( 0.300 \) \( \text{m} \)?
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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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