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Part of ME-02 — Kinematics

Formula Sheet — Kinematics

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Equations of Motion (constant acceleration)

v=u+at[LT−1]=[LT−1]+[LT−2][T]v = u + at \quad [LT^{-1}] = [LT^{-1}] + [LT^{-2}][T]

s=ut+12at2[L]=[LT−1][T]+[LT−2][T2]s = ut + \tfrac{1}{2}at^2 \quad [L] = [LT^{-1}][T] + [LT^{-2}][T^2]

v2=u2+2as[L2T−2]=[L2T−2]+[LT−2][L]v^2 = u^2 + 2as \quad [L^2T^{-2}] = [L^2T^{-2}] + [LT^{-2}][L]

sn=u+a(2n−1)2[L]=[LT−1]+[LT−2][T]s_n = u + \frac{a(2n-1)}{2} \quad [L] = [LT^{-1}] + [LT^{-2}][T]

Projectile Motion

T=2usin⁡θg[M0L0T1]=[LT−1][LT−2]T = \frac{2u\sin\theta}{g} \quad [M^0L^0T^1] = \frac{[LT^{-1}]}{[LT^{-2}]}

H=u2sin⁡2θ2g[M0L1T0]=[L2T−2][LT−2]H = \frac{u^2\sin^2\theta}{2g} \quad [M^0L^1T^0] = \frac{[L^2T^{-2}]}{[LT^{-2}]}

R=u2sin⁡2θg[M0L1T0]=[L2T−2][LT−2]R = \frac{u^2\sin 2\theta}{g} \quad [M^0L^1T^0] = \frac{[L^2T^{-2}]}{[LT^{-2}]}

Rmax=u2g at θ=45°R_{max} = \frac{u^2}{g} \text{ at } \theta = 45°

Vectors

Ax=Acos⁡θ,Ay=Asin⁡θ,A=Ax2+Ay2A_x = A\cos\theta, \quad A_y = A\sin\theta, \quad A = \sqrt{A_x^2 + A_y^2}

A⃗⋅B⃗=ABcos⁡θ(scalar)\vec{A}\cdot\vec{B} = AB\cos\theta \quad \text{(scalar)}

∣A⃗×B⃗∣=ABsin⁡θ(vector, direction by right-hand rule)|\vec{A}\times\vec{B}| = AB\sin\theta \quad \text{(vector, direction by right-hand rule)}

Circular Motion

ω=vr[M0L0T−1] (rad/s)\omega = \frac{v}{r} \quad [M^0L^0T^{-1}] \text{ (rad/s)}

ac=v2r=ω2r[M0L1T−2] (m/s2)a_c = \frac{v^2}{r} = \omega^2 r \quad [M^0L^1T^{-2}] \text{ (m/s}^2\text{)}

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