20 November 1997






Error Propagation
| Adding or Subtracting | Δ(A+B-C)= ΔA + ΔB + ΔC |
| Multiplying or Dividing | Δ(AB/C)= (AB/C)(ΔA/A + ΔB/B + ΔC/C) |
| Powers and Roots | Δ(Az) = zAz-1ΔA |
| Special Fuctions |
sin(θ±Δθ)
= sin(θ)±Δθ
cos(θ) cos(θ±Δθ) = cos(θ)±Δθ sin(θ) tan(θ±Δθ) = tan(θ)±Δθ /cos2(θ) e(x±Δx) = ex±Δxex ln(x±Δx) = ln(x)±Δx/x |
| Note: Δθ must be stated in radians! |
Kinematics
| vaverage = Δx/Δt | ωaverage = Δθ/Δt |
| vaverage = (vf+v0)/2 | ωaverage = (ωf+ ω0)/2 |
| aaverage = Δv/Δt | αaverage = Δω/Δt |
| Δx = vaveraget | Δθ = ωaveraget |
| Δx = v0t + ½at2 | Δθ = ω0t + ½αt2 |
| v = v0 + at | ω = ω0 + αt |
| v2 = (v0)2 + 2aΔx | ω2 = (ω0)2 + 2αΔθ |
Translation <-> Rotation
| s = Rθ | vtan = Rω | atan = Rα | ac = v2/R |
Newton's Laws
| ΣFx = max | ΣFy = may | fmax static = μsN | fkinetic = μkN |
| F = Gm1m1/R2 | g(R) = GMplanet/R2 | v = [GMplanet/R]½ | T2 = 4π2R2/ GMcentral | G = 6.672 × 10-11 N-m2/kg2 | g = 9.81 m/s2 |
Rolling
vlinear = vtangential
Torque
| τ = Iα | τ = r × F | τz = xFy - yFx |
Moment of Inertia
| Itotal = I1 + I2 + I3 ... | I = Icm + Md2 |
Work and Energy
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Klinear = ½mv2 | Krotational = ½Iω2 |
| Ugravity = mgh | Uspring = ½Kx2 |
Collisions
| p = mv | ![]() |
Pf = Pi |
| v1f - v1f = -(v1i - v2i) | I = Δp = FaverageΔt |
Angular Momentum
| L = r × p | Lz = xpy - ypx = rpsinφ | Llinear = bmv |
| Lorbital = r2mω | LA = IAωA | Ltotal = L1 + L2 + L3 ... |
| Lfinal = Linitial |
Simple Harmonic Motion
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Quadratic Formula
if ax2+bx+c = 0, then

Questions? mike.coombes@kwantlen.ca