Centripetal Forces, Universal Gravitation, and Satellite Motion Study Guide

Puck on a Frictionless Table: Top-Down and Side Views

  • System Setup: A puck of mass mm is tied to a fixed string and moves in a circular path at a constant speed on a frictionless horizontal tabletop.
  • Given Parameters:     * Mass (mm): 2kg2\,kg     * Speed (vv): 10m/s10\,m/s     * Radius (rr): 2m2\,m
  • Free Body Diagram (Side View): While the setup is often viewed from the top to see the path, the side view is essential for a Free Body Diagram (FBD):     * Normal Force (nn): Acts vertically upward from the table.     * Weight (mgmg): Acts vertically downward.     * Tension (TT): Acts horizontally toward the center of the circle.     * Acceleration (aca_c): Points toward the center of the circular path.
  • Applying Newton's Second Law:     * In the horizontal dimension, tension is the only force acting toward the center.     * Equation: T=m×acT = m \times a_c     * Substitute centripetal acceleration (ac=v2ra_c = \frac{v^2}{r}): T=m×v2rT = m \times \frac{v^2}{r}
  • Numerical Calculation:     * T=2kg×(10m/s)22mT = 2\,kg \times \frac{(10\,m/s)^2}{2\,m}     * T=2×1002=100NT = 2 \times \frac{100}{2} = 100\,N

Car Negotiating a Flat Horizontal Curve

  • Scenario: A 1500kg1500\,kg car travels through a curve on a flat road at a constant speed.
  • Given Parameters:     * Mass (mm): 1500kg1500\,kg     * Radius of Curvature (rr): 35m35\,m     * Coefficient of Static Friction (μs\mu_s): 0.50.5
  • Goal: Find the maximum speed (vmaxv_{max}) the car can maintain without skidding.
  • Radius of Curvature Defined: If the curve were extended to form a full circle, the radius of that circle would be 35m35\,m.
  • Friction Analysis:     * Type of Friction: Static friction (fsf_s) is used despite the car moving. This is because there is no relative motion between the point of contact of the tire and the road (unless the car is skidding).     * Maximum Static Friction: The limit right before skidding is fs,max=μs×nf_{s,max} = \mu_s \times n.
  • Free Body Diagram (Side View):     * Vertical: Normal force (nn) and weight (mgmg). Since there is no vertical acceleration, nmg=0n - mg = 0, so n=mgn = mg.     * Horizontal: The only force providing centripetal acceleration is static friction (fsf_s).
  • Newton's Second Law Equations:     * fs=m×ac=m×v2rf_s = m \times a_c = m \times \frac{v^2}{r}     * Substituing fs,maxf_{s,max}: μs×mg=m×v2r\mu_s \times mg = m \times \frac{v^2}{r}     * Mass (mm) cancels from both sides: μs×g=v2r\mu_s \times g = \frac{v^2}{r}     * Solving for speed: v=μs×r×gv = \sqrt{\mu_s \times r \times g}
  • Numerical Calculation:     * v=0.5×35m×9.8m/s2v = \sqrt{0.5 \times 35\,m \times 9.8\,m/s^2}     * v13.1m/sv \approx 13.1\,m/s

Banked Curves and Design Speed

  • Concept: A banked curve is a road slanted toward the inside of the curve. This design allows cars to negotiate turns even when the road is perfectly icy (frictionless).
  • Scenario (Icy Road Logic): An exit ramp is banked at an angle θ\theta so that a car can maintain its path without relying on friction at a specific speed.
  • Given Parameters:     * Designated Speed (vv): 13.4m/s13.4\,m/s     * Radius of Curvature (rr): 50m50\,m
  • Goal: Find the bank angle (θ\theta).
  • Coordinate System Selection: Select axes such that the x-axis points toward the center of the circle (the direction of centripetal acceleration). This prevents the need to break acceleration into components.
  • Free Body Diagram (Frictionless Case):     * Weight (mgmg): Points straight down.     * Normal Force (nn): Points perpendicular to the slanted road surface.
  • Geometric Relationship: The angle θ\theta between the horizontal and the road is the same as the angle between the vertical (y-axis) and the normal force.
  • Equations from Newton's Second Law:     * Vertical (yy): ncos(θ)mg=0n=mgcos(θ)n \cos(\theta) - mg = 0 \rightarrow n = \frac{mg}{\cos(\theta)}     * Horizontal (xx): nsin(θ)=m×ac=m×v2rn \sin(\theta) = m \times a_c = m \times \frac{v^2}{r}
  • Combining Equations:     * Substitute nn: (mgcos(θ))×sin(θ)=m×v2r(\frac{mg}{\cos(\theta)}) \times \sin(\theta) = m \times \frac{v^2}{r}     * Mass (mm) cancels: g×tan(θ)=v2rg \times \tan(\theta) = \frac{v^2}{r}     * Solve for angle: θ=arctan(v2r×g)\theta = \arctan(\frac{v^2}{r \times g})
  • Numerical Calculation:     * θ=arctan((13.4m/s)250m×9.8m/s2)\theta = \arctan(\frac{(13.4\,m/s)^2}{50\,m \times 9.8\,m/s^2})     * θ20.1\theta \approx 20.1^{\circ}
  • Motion Dynamics: If speed is less than 13.4m/s13.4\,m/s, the car tends to slide down the bank; if speed is greater, it tends to slide up and off the road.

Pilot in a Vertical Loop (Airplane Trick)

  • Scenario: An airplane performs a vertical loop of radius rr at a constant speed vv.
  • Given Parameters:     * Radius (rr): 2.7km=2700m2.7\,km = 2700\,m     * Speed (vv): 225m/s225\,m/s
  • Goal: Determine the normal force (nn) exerted by the seat on the pilot at the top and bottom of the loop in terms of pilot weight (mgmg).
  • Case 1: Top of the Loop:     * FBD: The plane is upside down. Weight (mgmg) is down. Normal force (nn) is down. Centripetal acceleration (aca_c) is down.     * Equation: n+mg=m×v2rn + mg = m \times \frac{v^2}{r}     * Solve for nn: n=m(v2rg)n = m(\frac{v^2}{r} - g)     * In terms of weight: Factor out gg to get n=mg(v2rg1)n = mg(\frac{v^2}{rg} - 1).     * Calculation: n=mg(22522700×9.81)0.913×mgn = mg(\frac{225^2}{2700 \times 9.8} - 1) \approx 0.913 \times mg (91.3%91.3\% of pilot's weight).
  • Case 2: Bottom of the Loop:     * FBD: The plane is upright. Weight (mgmg) is down. Normal force (nn) is up. Centripetal acceleration (aca_c) is up.     * Equation: nmg=m×v2rn - mg = m \times \frac{v^2}{r}     * Solve for nn: n=m(v2r+g)n = m(\frac{v^2}{r} + g)     * In terms of weight: Factor out gg to get n=mg(v2rg+1)n = mg(\frac{v^2}{rg} + 1).     * Calculation: n=mg(22522700×9.8+1)2.91×mgn = mg(\frac{225^2}{2700 \times 9.8} + 1) \approx 2.91 \times mg (nearly 33 times the pilot's weight).

Universal Gravitation

  • Definition: The gravitational force between any two objects in the universe is attractive and depends on their masses and the distance between their centers of gravity.
  • Universal Gravitation Formula: F=G×m1×m2r2F = G \times \frac{m_1 \times m_2}{r^2}
  • Gravitational Constant (GG): G6.67×1011Nm2/kg2G \approx 6.67 \times 10^{-11}\,N\,m^2/kg^2
  • Distance (rr): Measured from the center of gravity of one object to the center of gravity of the second object.
  • Application to Earth's Surface:     * F=G×ME×mRE2F = G \times \frac{M_E \times m}{R_E^2}, where MEM_E is Earth's mass and RER_E is Earth's radius.     * The term G×MERE2\frac{G \times M_E}{R_E^2} simplifies to g=9.8m/s2g = 9.8\,m/s^2, allowing for the local weight formula F=mgF = mg.

Satellite Motion

  • Dynamics: A satellite in orbit is kept in a circular path by the gravitational force of the Earth, which acts as the centripetal force.
  • Newton's Second Law for Satellites:     * G×ME×msr2=ms×v2rG \times \frac{M_E \times m_s}{r^2} = m_s \times \frac{v^2}{r}     * Mass of the satellite (msm_s) cancels.
  • Orbital Speed (vv):     * v=G×MErv = \sqrt{\frac{G \times M_E}{r}}     * Orbit radius r=RE+hr = R_E + h, where hh is the height above the Earth's surface.
  • Substitutions with Period (TT):     * For a constant speed circular orbit, v=2πrTv = \frac{2\pi r}{T}.     * Substitute into the force equation: G×MEr=v2=(2πrT)2G \times \frac{M_E}{r} = v^2 = (\frac{2\pi r}{T})^2     * Resulting Relation: G×MEr=4π2r2T2G \times \frac{M_E}{r} = \frac{4\pi^2 r^2}{T^2}
  • Kepler's Third Law: The derivation leads to the relationship where the square of the period is proportional to the cube of the radius (T2r3T^2 \propto r^3). For elliptical orbits, rr is replaced by the semi-major axis.