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| Derivation/Formula | Reasoning |
|---|---|
| \[v_i\sin\theta = 25(0.602)=15.0\,\text{m/s}\] | Resolve the launch speed into the vertical component using \(\sin37^\circ\approx0.602\). |
| \[\Delta y = v_i\sin\theta\,t – \tfrac12 g t^2\] | Use the vertical displacement equation with \(\Delta y = +5.0\,\text{m}\) and \(g=9.8\,\text{m/s}^2\). |
| \[4.9t^2-15.0t+5.0=0\] | Substitute numerical values and rearrange to standard quadratic form. |
| \[t=\frac{15.0\pm11.3}{9.8}\] | Apply the quadratic formula: \(t=\tfrac{-b\pm\sqrt{b^2-4ac}}{2a}\). |
| \[t=0.38\,\text{s}\quad\text{or}\quad t=2.69\,\text{s}\] | The smaller root is when the projectile is still rising; the larger root is the total flight time. |
| \[\boxed{t=2.69\,\text{s}}\] | Total time aloft. |
| Derivation/Formula | Reasoning |
|---|---|
| \[v_i\cos\theta = 25(0.799)=20.0\,\text{m/s}\] | Resolve the launch speed into the constant horizontal component using \(\cos37^\circ\approx0.799\). |
| \[\Delta x = v_i\cos\theta\;t\] | Horizontal displacement equals horizontal velocity times time; no horizontal acceleration. |
| \[\Delta x = 20.0\times2.69 = 5.38\times10^{1}\,\text{m}\] | Insert \(t=2.69\,\text{s}\) from part (a). |
| \[\boxed{\Delta x = 53.8\,\text{m}}\] | Horizontal range. |
| Derivation/Formula | Reasoning |
|---|---|
| \[v_{y\,(\text{top})}=0\,\text{m/s}\] | At the highest point the vertical component of velocity is momentarily zero for any projectile motion neglecting air resistance. |
| \[\boxed{0\,\text{m/s}}\] | Result. |
| Derivation/Formula | Reasoning |
|---|---|
| \[v_{y\,(\text{land})}=v_i\sin\theta – g t = 15.0 – 9.8(2.69) = -11.3\,\text{m/s}\] | Vertical velocity after \(t=2.69\,\text{s}\); negative sign indicates downward direction. |
| \[v_{x}=20.0\,\text{m/s}\] | Horizontal velocity is unchanged throughout flight. |
| \[v_x^2 = v_{y\,(\text{land})}^2 + (v_{x})^2 = (11.3)^2 + (20.0)^2 = 5.27\times10^{2}\] | Pythagorean addition of components for speed magnitude (labelled here as \(v_x\) per notation). |
| \[v_x = 22.9\,\text{m/s}\] | Square-root of previous result. |
| \[\boxed{v_x < v_i}\] | The landing speed \(22.9\,\text{m/s}\) is less than the launch speed \(25\,\text{m/s}\) because the projectile finishes 5 m higher, converting some kinetic energy into gravitational potential energy. |
Just ask: "Help me solve this problem."
You drop a rock off a bridge. When the rock has fallen \( 4 \) \( \text{m} \), you drop a second rock. As the two rocks continue to fall, what happens to their velocities?
In a lab experiment, a ball is rolled down a ramp so that it leaves the edge of the table with a horizontal velocity [katex]v[/katex]. Assume there are no frictional forces. If the table has a height [katex]h[/katex] above the ground, how far away from the edge of the table, a distance [katex]x[/katex], does the ball land?
An object can move upward while having a downward acceleration.
A javelin thrower, of height \( 1.8 \) \( \text{m} \), throws a javelin with initial velocity of \( 26 \) \( \text{m s}^{-1} \) at \( 38^{\circ} \) to the horizontal. Calculate the time taken for the javelin to reach the ground from its maximum height. Give your answer in seconds and to an appropriate number of significant figures.
Projectiles 1 and 2 are launched from level ground at the same time and follow the trajectories shown in the figure. Which one of the projectiles, if either, returns to the ground first, and why?
\(2.69\,\text{s}\)
\(53.8\,\text{m}\)
\(0\,\text{m/s}\)
\(v_x < v_i\)
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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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