Comprehensive Physics Study Guide: Classical Mechanics, Kinematics, and Dynamics

Static Equilibrium in Multi-Rope Systems

  • Static equilibrium requires that both the net horizontal force and net vertical force acting on a system equal zero:   ∑Fx=0\sum F_x = 0∑Fy=0\sum F_y = 0

Circus performer clinging to trapeze with tension forces T1 and T2

System Setup and Parameters

  • Mass of performer: m=76.0 kgm = 76.0\,\text{kg}
  • Gravitational acceleration: g=9.80 m/s2g = 9.80\,\text{m/s}^2
  • Downward weight force: w=mg=76.0 kg×9.80 m/s2=744.8 Nw = m g = 76.0\,\text{kg} \times 9.80\,\text{m/s}^2 = 744.8\,\text{N}
  • Rope 1 tension (T1T_1): Oriented at an angle of 15∘15^\circ relative to the vertical line.
  • Rope 2 tension (T2T_2): Oriented at an angle of 10∘10^\circ above the horizontal line.

Force Component Equations

  • Horizontal force equilibrium:   T2cos⁡(10∘)−T1sin⁡(15∘)=0T_2 \cos(10^\circ) - T_1 \sin(15^\circ) = 0T1sin⁡(15∘)=T2cos⁡(10∘)T_1 \sin(15^\circ) = T_2 \cos(10^\circ)
  • Vertical force equilibrium:   T1cos⁡(15∘)+T2sin⁡(10∘)−w=0T_1 \cos(15^\circ) + T_2 \sin(10^\circ) - w = 0T1cos⁡(15∘)+T2sin⁡(10∘)=744.8 NT_1 \cos(15^\circ) + T_2 \sin(10^\circ) = 744.8\,\text{N}

Step-by-Step Derivation and Calculation

  • Express T1T_1 in terms of T2T_2 using horizontal force balance:   T1=T2cos⁡(10∘)sin⁡(15∘)T_1 = T_2 \frac{\cos(10^\circ)}{\sin(15^\circ)}T1=T2×0.984810.25882≈3.8050T2T_1 = T_2 \times \frac{0.98481}{0.25882} \approx 3.8050 T_2
  • Substitute T1T_1 into the vertical force equilibrium equation:   (3.8050T2)cos⁡(15∘)+T2sin⁡(10∘)=744.8 N(3.8050 T_2) \cos(15^\circ) + T_2 \sin(10^\circ) = 744.8\,\text{N}3.8050T2(0.96593)+0.17365T2=744.8 N3.8050 T_2 (0.96593) + 0.17365 T_2 = 744.8\,\text{N}3.6754T2+0.17365T2=744.8 N3.6754 T_2 + 0.17365 T_2 = 744.8\,\text{N}3.8490T2=744.8 N3.8490 T_2 = 744.8\,\text{N}T2=744.8 N3.8490≈193.5 NT_2 = \frac{744.8\,\text{N}}{3.8490} \approx 193.5\,\text{N}
  • Calculate T1T_1:   T1=3.8050×193.5 N≈736.3 NT_1 = 3.8050 \times 193.5\,\text{N} \approx 736.3\,\text{N}

One-Dimensional Kinematics and Elevator Dynamics

  • The vertical motion of an elevator supported by a cable is governed by Newton's second law along the vertical axis:   ∑Fy=T−mg=ma\sum F_y = T - m g = m aT=m(g+a)T = m(g + a)

System Parameters

  • Mass of elevator and passengers: m=1.7×103 kg=1700 kgm = 1.7 \times 10^3\,\text{kg} = 1700\,\text{kg}
  • Acceleration due to gravity: g=9.80 m/s2g = 9.80\,\text{m/s}^2

Phase (a): Upward Acceleration from Rest

  • Acceleration: a1=1.20 m/s2a_1 = 1.20\,\text{m/s}^2 upward for duration t1=1.50 st_1 = 1.50\,\text{s}.
  • Cable tension calculation:   Ta=m(g+a1)T_a = m(g + a_1)Ta=(1.7×103 kg)×(9.80 m/s2+1.20 m/s2)=1700 kg×11.00 m/s2=18700 N=1.87×104 NT_a = (1.7 \times 10^3\,\text{kg}) \times (9.80\,\text{m/s}^2 + 1.20\,\text{m/s}^2) = 1700\,\text{kg} \times 11.00\,\text{m/s}^2 = 18700\,\text{N} = 1.87 \times 10^4\,\text{N}

Phase (b): Constant Velocity Motion

  • Acceleration: a2=0 m/s2a_2 = 0\,\text{m/s}^2 for duration t2=8.50 st_2 = 8.50\,\text{s}.
  • Cable tension calculation:   Tb=mgT_b = m gTb=(1.7×103 kg)×9.80 m/s2=16660 N=1.67×104 NT_b = (1.7 \times 10^3\,\text{kg}) \times 9.80\,\text{m/s}^2 = 16660\,\text{N} = 1.67 \times 10^4\,\text{N}

Phase (c): Deceleration (Acceleration Opposite to Motion)

  • Acceleration: a3=−0.600 m/s2a_3 = -0.600\,\text{m/s}^2 for duration t3=3.00 st_3 = 3.00\,\text{s}.
  • Cable tension calculation:   Tc=m(g+a3)T_c = m(g + a_3)Tc=(1.7×103 kg)×(9.80 m/s2−0.600 m/s2)=1700 kg×9.20 m/s2=15640 N=1.56×104 NT_c = (1.7 \times 10^3\,\text{kg}) \times (9.80\,\text{m/s}^2 - 0.600\,\text{m/s}^2) = 1700\,\text{kg} \times 9.20\,\text{m/s}^2 = 15640\,\text{N} = 1.56 \times 10^4\,\text{N}

Phase (d): Displacement and Velocity Analysis

  • Velocity after Phase 1:   v1=v0+a1t1=0 m/s+(1.20 m/s2)(1.50 s)=1.80 m/sv_1 = v_0 + a_1 t_1 = 0\,\text{m/s} + (1.20\,\text{m/s}^2)(1.50\,\text{s}) = 1.80\,\text{m/s}
  • Displacement during Phase 1:   Δy1=v0t1+12a1t12=0+12(1.20 m/s2)(1.50 s)2=1.35 m\Delta y_1 = v_0 t_1 + \frac{1}{2} a_1 t_1^2 = 0 + \frac{1}{2}(1.20\,\text{m/s}^2)(1.50\,\text{s})^2 = 1.35\,\text{m}
  • Velocity after Phase 2:   v2=v1=1.80 m/sv_2 = v_1 = 1.80\,\text{m/s}
  • Displacement during Phase 2:   Δy2=v1t2=(1.80 m/s)(8.50 s)=15.3 m\Delta y_2 = v_1 t_2 = (1.80\,\text{m/s})(8.50\,\text{s}) = 15.3\,\text{m}
  • Final velocity after Phase 3:   vf=v2+a3t3=1.80 m/s+(−0.600 m/s2)(3.00 s)=1.80 m/s−1.80 m/s=0 m/sv_f = v_2 + a_3 t_3 = 1.80\,\text{m/s} + (-0.600\,\text{m/s}^2)(3.00\,\text{s}) = 1.80\,\text{m/s} - 1.80\,\text{m/s} = 0\,\text{m/s}
  • Displacement during Phase 3:   Δy3=v2t3+12a3t32=(1.80 m/s)(3.00 s)+12(−0.600 m/s2)(3.00 s)2=5.40 m−2.70 m=2.70 m\Delta y_3 = v_2 t_3 + \frac{1}{2} a_3 t_3^2 = (1.80\,\text{m/s})(3.00\,\text{s}) + \frac{1}{2}(-0.600\,\text{m/s}^2)(3.00\,\text{s})^2 = 5.40\,\text{m} - 2.70\,\text{m} = 2.70\,\text{m}
  • Total height moved above starting point:   Δytotal=Δy1+Δy2+Δy3=1.35 m+15.3 m+2.70 m=19.35 m\Delta y_{\text{total}} = \Delta y_1 + \Delta y_2 + \Delta y_3 = 1.35\,\text{m} + 15.3\,\text{m} + 2.70\,\text{m} = 19.35\,\text{m}
  • Final velocity: vf=0 m/sv_f = 0\,\text{m/s}

Frictionless Inclined Plane Motion

  • On a frictionless incline inclined at angle θ\theta to the horizontal, the force component parallel to the incline is mgsin⁡(θ)m g \sin(\theta).

System Parameters

  • Length of track: d=30.0 md = 30.0\,\text{m}
  • Incline angle: θ=20.0∘\theta = 20.0^\circ
  • Initial speed: v0=0 m/sv_0 = 0\,\text{m/s}
  • Acceleration of gravity: g=9.80 m/s2g = 9.80\,\text{m/s}^2

(a) Acceleration Along the Incline

  • Formula:   a=gsin⁡(θ)a = g \sin(\theta)
  • Calculation:   a=9.80 m/s2×sin⁡(20.0∘)=9.80 m/s2×0.34202≈3.35 m/s2a = 9.80\,\text{m/s}^2 \times \sin(20.0^\circ) = 9.80\,\text{m/s}^2 \times 0.34202 \approx 3.35\,\text{m/s}^2

(b) Elapsed Time Calculation

  • Kinematic equation:   d=v0t+12at2d = v_0 t + \frac{1}{2} a t^230.0 m=0+12(3.3518 m/s2)t230.0\,\text{m} = 0 + \frac{1}{2} (3.3518\,\text{m/s}^2) t^2t2=2×30.0 m3.3518 m/s2≈17.8998t^2 = \frac{2 \times 30.0\,\text{m}}{3.3518\,\text{m/s}^2} \approx 17.8998t=17.8998≈4.23 st = \sqrt{17.8998} \approx 4.23\,\text{s}

Force Analysis and Static Equilibrium in Rock Climbing

Mountain climber supported by rope and feet pushing against rock face

System Parameters

  • Mass of climber: m=52.0 kgm = 52.0\,\text{kg}
  • Climber weight: w=mg=52.0 kg×9.80 m/s2=509.6 Nw = m g = 52.0\,\text{kg} \times 9.80\,\text{m/s}^2 = 509.6\,\text{N}
  • Rope angle with vertical cliff face: θrope=31∘\theta_{\text{rope}} = 31^\circ
  • Leg force angle relative to horizontal: θlegs=15∘\theta_{\text{legs}} = 15^\circ

(a) Tension and Leg Force Calculations

  • Horizontal force equilibrium (taking horizontal axis perpendicular to the cliff):   Flegscos⁡(15∘)−Tsin⁡(31∘)=0F_{\text{legs}} \cos(15^\circ) - T \sin(31^\circ) = 0Flegs=Tsin⁡(31∘)cos⁡(15∘)F_{\text{legs}} = T \frac{\sin(31^\circ)}{\cos(15^\circ)}
  • Vertical force equilibrium:   Tcos⁡(31∘)+Flegssin⁡(15∘)−w=0T \cos(31^\circ) + F_{\text{legs}} \sin(15^\circ) - w = 0
  • Substitute leg force expression into vertical equation:   Tcos⁡(31∘)+Tsin⁡(31∘)sin⁡(15∘)cos⁡(15∘)=wT \cos(31^\circ) + T \frac{\sin(31^\circ) \sin(15^\circ)}{\cos(15^\circ)} = wT(cos⁡(31∘)+sin⁡(31∘)tan⁡(15∘))=509.6 NT \left( \cos(31^\circ) + \sin(31^\circ) \tan(15^\circ) \right) = 509.6\,\text{N}T(0.85717+0.51504×0.26795)=509.6 NT (0.85717 + 0.51504 \times 0.26795) = 509.6\,\text{N}T(0.85717+0.13800)=509.6 NT (0.85717 + 0.13800) = 509.6\,\text{N}T(0.99517)=509.6 N  ⟹  T≈512 NT (0.99517) = 509.6\,\text{N} \implies T \approx 512\,\text{N}
  • Compute force exerted parallel to legs (FlegsF_{\text{legs}}):   Flegs=512.07 N×sin⁡(31∘)cos⁡(15∘)=512.07 N×0.515040.96593≈273 NF_{\text{legs}} = 512.07\,\text{N} \times \frac{\sin(31^\circ)}{\cos(15^\circ)} = 512.07\,\text{N} \times \frac{0.51504}{0.96593} \approx 273\,\text{N}

(b) Minimum Coefficient of Static Friction

  • The leg force exerted against the cliff face has a normal component NN perpendicular to the cliff and a tangential friction force fsf_s parallel to the cliff face:   N=Flegscos⁡(15∘)N = F_{\text{legs}} \cos(15^\circ)fs=Flegssin⁡(15∘)f_s = F_{\text{legs}} \sin(15^\circ)
  • Minimum static coefficient of friction condition:   μs,min=fsN=Flegssin⁡(15∘)Flegscos⁡(15∘)=tan⁡(15∘)≈0.268\mu_{s,\text{min}} = \frac{f_s}{N} = \frac{F_{\text{legs}} \sin(15^\circ)}{F_{\text{legs}} \cos(15^\circ)} = \tan(15^\circ) \approx 0.268

Vehicle Acceleration Dynamics on Inclined Slopes with Friction Limits

  • When a vehicle accelerates up a slope, the driving force is provided by static friction at the drive wheels.

General Governing Equation

  • Slope angle: θ=4.00∘\theta = 4.00^\circ
  • Normal force on drive wheels (supporting half the total weight):   Ndrive=12mgcos⁡(4.00∘)N_{\text{drive}} = \frac{1}{2} m g \cos(4.00^\circ)
  • Maximum available static friction force:   fs,max=μsNdrive=12μsmgcos⁡(4.00∘)f_{s,\text{max}} = \mu_s N_{\text{drive}} = \frac{1}{2} \mu_s m g \cos(4.00^\circ)
  • Acceleration balance along incline:   fs,max−mgsin⁡(4.00∘)=mamaxf_{s,\text{max}} - m g \sin(4.00^\circ) = m a_{\text{max}}amax=g(12μscos⁡(4.00∘)−sin⁡(4.00∘))a_{\text{max}} = g \left( \frac{1}{2} \mu_s \cos(4.00^\circ) - \sin(4.00^\circ) \right)
  • Numerical constant values:   cos⁡(4.00∘)≈0.99756\cos(4.00^\circ) \approx 0.99756sin⁡(4.00∘)≈0.06976\sin(4.00^\circ) \approx 0.06976g=9.80 m/s2g = 9.80\,\text{m/s}^2

(a) Acceleration on Dry Concrete (μs=1.0\mu_s = 1.0)

  • Calculation:   amax=9.80 m/s2×(0.5×1.0×0.99756−0.06976)a_{\text{max}} = 9.80\,\text{m/s}^2 \times \left( 0.5 \times 1.0 \times 0.99756 - 0.06976 \right)amax=9.80×(0.49878−0.06976)=9.80×0.42902≈4.20 m/s2a_{\text{max}} = 9.80 \times (0.49878 - 0.06976) = 9.80 \times 0.42902 \approx 4.20\,\text{m/s}^2

(b) Acceleration on Wet Concrete (μs=0.7\mu_s = 0.7)

  • Calculation:   amax=9.80 m/s2×(0.5×0.7×0.99756−0.06976)a_{\text{max}} = 9.80\,\text{m/s}^2 \times \left( 0.5 \times 0.7 \times 0.99756 - 0.06976 \right)amax=9.80×(0.27932−0.06976)=9.80×0.20956≈2.05 m/s2a_{\text{max}} = 9.80 \times (0.27932 - 0.06976) = 9.80 \times 0.20956 \approx 2.05\,\text{m/s}^2

(c) Acceleration on Ice (μs=0.100\mu_s = 0.100)

  • Calculation:   amax=9.80 m/s2×(0.5×0.100×0.99756−0.06976)a_{\text{max}} = 9.80\,\text{m/s}^2 \times \left( 0.5 \times 0.100 \times 0.99756 - 0.06976 \right)amax=9.80×(0.04988−0.06976)=9.80×(−0.01988)≈−0.195 m/s2a_{\text{max}} = 9.80 \times (0.04988 - 0.06976) = 9.80 \times (-0.01988) \approx -0.195\,\text{m/s}^2
  • Physical Meaning: The negative value demonstrates that static friction is insufficient to counteract gravity down the incline; the vehicle cannot accelerate Uphill and will slide backwards.

Centripetal Force and Seat Normal Force in Vertical Circular Loops

Roller coaster car traversing circular loop with points A and B highlighted

System Parameters

  • Mass of child: m=40.0 kgm = 40.0\,\text{kg}
  • Radius of circular loop: r=7.00 mr = 7.00\,\text{m}
  • Speed at Point A (top of loop): vA=10.0 m/sv_A = 10.0\,\text{m/s}
  • Speed at Point B (30∘30^\circ past top of loop): vB=10.5 m/sv_B = 10.5\,\text{m/s}

(a) Force of Car Seat on Child at Point A

  • At the top of the loop, both normal force NAN_A and gravity mgm g point downward toward the loop center:   NA+mg=mvA2rN_A + m g = \frac{m v_A^2}{r}NA=m(vA2r−g)N_A = m \left( \frac{v_A^2}{r} - g \right)
  • Computation:   NA=40.0 kg×((10.0 m/s)27.00 m−9.80 m/s2)N_A = 40.0\,\text{kg} \times \left( \frac{(10.0\,\text{m/s})^2}{7.00\,\text{m}} - 9.80\,\text{m/s}^2 \right)NA=40.0×(14.286−9.80)=40.0×4.486≈179 NN_A = 40.0 \times (14.286 - 9.80) = 40.0 \times 4.486 \approx 179\,\text{N}

(b) Force of Car Seat on Child at Point B

  • Point B is positioned at an angle θ=30.0∘\theta = 30.0^\circ from vertical. Radial inward gravitational component is mgcos⁡(30∘)m g \cos(30^\circ):   NB+mgcos⁡(30∘)=mvB2rN_B + m g \cos(30^\circ) = \frac{m v_B^2}{r}NB=m(vB2r−gcos⁡(30∘))N_B = m \left( \frac{v_B^2}{r} - g \cos(30^\circ) \right)
  • Computation:   vB2r=(10.5 m/s)27.00 m=110.257.00=15.75 m/s2\frac{v_B^2}{r} = \frac{(10.5\,\text{m/s})^2}{7.00\,\text{m}} = \frac{110.25}{7.00} = 15.75\,\text{m/s}^2gcos⁡(30∘)=9.80 m/s2×0.86603=8.487 m/s2g \cos(30^\circ) = 9.80\,\text{m/s}^2 \times 0.86603 = 8.487\,\text{m/s}^2NB=40.0 kg×(15.75 m/s2−8.487 m/s2)=40.0×7.263≈291 NN_B = 40.0\,\text{kg} \times (15.75\,\text{m/s}^2 - 8.487\,\text{m/s}^2) = 40.0 \times 7.263 \approx 291\,\text{N}

(c) Minimum Speed Required at Point A to Remain in Seat

  • The child remains in contact with the seat as long as NA≥0N_A \ge 0. Threshold velocity occurs when NA=0N_A = 0:   mvmin2r=mg\frac{m v_{\text{min}}^2}{r} = m gvmin=grv_{\text{min}} = \sqrt{g r}
  • Computation:   vmin=9.80 m/s2×7.00 m=68.6≈8.28 m/sv_{\text{min}} = \sqrt{9.80\,\text{m/s}^2 \times 7.00\,\text{m}} = \sqrt{68.6} \approx 8.28\,\text{m/s}

Maximum Traversing Speed on Unbanked Curves

  • On an unbanked flat curve, centripetal force is supplied entirely by static friction between tires and road.

System Parameters

  • Radius of unbanked curve: r=65 mr = 65\,\text{m}
  • Coefficient of static friction: μs=0.70\mu_s = 0.70
  • Gravitational acceleration: g=9.80 m/s2g = 9.80\,\text{m/s}^2

Derivation and Speed Calculation

  • Friction force balance:   fs,max=μsN=μsmgf_{s,\text{max}} = \mu_s N = \mu_s m gmvmax2r=μsmg\frac{m v_{\text{max}}^2}{r} = \mu_s m gvmax=μsgrv_{\text{max}} = \sqrt{\mu_s g r}
  • Computation:   vmax=0.70×9.80 m/s2×65 m=445.9≈21.1 m/sv_{\text{max}} = \sqrt{0.70 \times 9.80\,\text{m/s}^2 \times 65\,\text{m}} = \sqrt{445.9} \approx 21.1\,\text{m/s}

Dynamics of Ideally Banked Circular Turns

  • An ideally banked curve allows a vehicle to make a turn at a specific speed without relying on friction forces.

System Parameters

  • Bank angle: θ=75.0∘\theta = 75.0^\circ
  • Bobsled speed: v=30.0 m/sv = 30.0\,\text{m/s}
  • Acceleration of gravity: g=9.80 m/s2g = 9.80\,\text{m/s}^2

(a) Radius of the Turn

  • Relationship for ideal banking angle:   tan⁡(θ)=v2gr\tan(\theta) = \frac{v^2}{g r}r=v2gtan⁡(θ)r = \frac{v^2}{g \tan(\theta)}
  • Computation:   tan⁡(75.0∘)≈3.73205\tan(75.0^\circ) \approx 3.73205r=(30.0 m/s)29.80 m/s2×3.73205=90036.574≈24.6 mr = \frac{(30.0\,\text{m/s})^2}{9.80\,\text{m/s}^2 \times 3.73205} = \frac{900}{36.574} \approx 24.6\,\text{m}

(b) Centripetal Acceleration

  • Formula:   ac=v2r=gtan⁡(θ)a_c = \frac{v^2}{r} = g \tan(\theta)
  • Computation:   ac=9.80 m/s2×tan⁡(75.0∘)=9.80×3.73205≈36.6 m/s2a_c = 9.80\,\text{m/s}^2 \times \tan(75.0^\circ) = 9.80 \times 3.73205 \approx 36.6\,\text{m/s}^2

(c) Acceleration Expressed in g's

  • Conversion:   Acceleration in g’s=acg=tan⁡(75.0∘)≈3.73 g\text{Acceleration in g's} = \frac{a_c}{g} = \tan(75.0^\circ) \approx 3.73\,\text{g}

Fluid Drag and Terminal Velocity Analysis

  • Falling objects reach terminal velocity when resistive air drag force equals object weight.

Drag Force Governing Model

  • Drag force formula:   Fd=12ρCAv2F_d = \frac{1}{2} \rho C A v^2   where:
    • ρ\rho is fluid density.
    • CC is dimensionless drag coefficient.
    • AA is cross-sectional frontal area.
    • vv is velocity relative to fluid.

System Parameters

  • Skydiver mass: m=80.0 kgm = 80.0\,\text{kg}
  • Cross-sectional area in pike position: A=0.14 m2A = 0.14\,\text{m}^2
  • Drag coefficient: C=0.70C = 0.70
  • Air density: ρ=1.21 kg/m3\rho = 1.21\,\text{kg/m}^3
  • Gravitational acceleration: g=9.80 m/s2g = 9.80\,\text{m/s}^2

Terminal Velocity Derivation and Calculation

  • Force balance at terminal speed (vtv_t):   Fd=mgF_d = m g12ρCAvt2=mg\frac{1}{2} \rho C A v_t^2 = m gvt=2mgρCAv_t = \sqrt{\frac{2 m g}{\rho C A}}
  • Numerical substitution:   2mg=2×80.0 kg×9.80 m/s2=1568 N2 m g = 2 \times 80.0\,\text{kg} \times 9.80\,\text{m/s}^2 = 1568\,\text{N}ρCA=1.21 kg/m3×0.70×0.14 m2=0.11858 kg/m\rho C A = 1.21\,\text{kg/m}^3 \times 0.70 \times 0.14\,\text{m}^2 = 0.11858\,\text{kg/m}vt=1568 N0.11858 kg/m=13223.14≈115 m/sv_t = \sqrt{\frac{1568\,\text{N}}{0.11858\,\text{kg/m}}} = \sqrt{13223.14} \approx 115\,\text{m/s}