Skip to main content

Radial and transverse components of acceleration

Short answer

Velocity components: v_r = ṙ, v_θ = rθ̇. Acceleration: a_r = r̈ – rθ̇², a_θ = rθ̈ + 2ṙθ̇. Equations of motion: ΣF_r = m(r̈ – rθ̇²), ΣF_θ = m(rθ̈ + 2ṙθ̇). For central forces, angular momentum r²θ̇ is constant.

Derive expressions for the radial and transverse components of velocity and acceleration of a particle moving along a plane curve. Hence write the equations of motion of the particle in polar coordinates.

Polar coordinates (r,θ)(r,\theta) locate a particle by its distance rr from the pole O and the angle θ\theta of the radius vector from a fixed line. Two unit vectors are used: er\mathbf{e}_r along the radius vector and eθ\mathbf{e}_\theta perpendicular to it (in the direction of increasing θ\theta).

          y
          |      P
          |    / |
          |  /   | e_theta
          | / r  |-> e_r
          |/ th
     O----+------------ x

Rate of change of unit vectors

Because the directions of er\mathbf{e}_r and eθ\mathbf{e}_\theta rotate with θ\theta:

e˙r=θ˙ eθe˙θ=−θ˙ er\dot{\mathbf{e}}_r = \dot\theta\,\mathbf{e}_\theta \qquad \dot{\mathbf{e}}_\theta = -\dot\theta\,\mathbf{e}_r

Velocity

The position vector is r=r er\mathbf{r} = r\,\mathbf{e}_r. Differentiating:

v=r˙ er+re˙r=r˙ er+rθ˙ eθ\mathbf{v} = \dot r\,\mathbf{e}_r + r\dot{\mathbf{e}}_r = \dot r\,\mathbf{e}_r + r\dot\theta\,\mathbf{e}_\theta

So vr=r˙v_r = \dot r (radial) and vθ=rθ˙v_\theta = r\dot\theta (transverse), with v=vr2+vθ2v = \sqrt{v_r^2 + v_\theta^2}.

Acceleration

Differentiating again:

a=r¨ er+r˙θ˙ eθ+(r˙θ˙+rθ¨) eθ−rθ˙2 er=(r¨−rθ˙2) er+(rθ¨+2r˙θ˙) eθ\begin{aligned} \mathbf{a} &= \ddot r\,\mathbf{e}_r + \dot r\dot\theta\,\mathbf{e}_\theta + (\dot r\dot\theta + r\ddot\theta)\,\mathbf{e}_\theta - r\dot\theta^2\,\mathbf{e}_r \\ &= (\ddot r - r\dot\theta^2)\,\mathbf{e}_r + (r\ddot\theta + 2\dot r\dot\theta)\,\mathbf{e}_\theta \end{aligned} ar=r¨−rθ˙2aθ=rθ¨+2r˙θ˙a_r = \ddot r - r\dot\theta^2 \qquad a_\theta = r\ddot\theta + 2\dot r\dot\theta

The term 2r˙θ˙2\dot r\dot\theta is the Coriolis component; rθ˙2r\dot\theta^2 is the centripetal term.

Equations of motion

Applying Newton's second law ΣF=ma\Sigma \mathbf{F} = m\mathbf{a} along the two directions:

ΣFr=m(r¨−rθ˙2)ΣFθ=m(rθ¨+2r˙θ˙)\Sigma F_r = m(\ddot r - r\dot\theta^2) \qquad \Sigma F_\theta = m(r\ddot\theta + 2\dot r\dot\theta)

For a central force (ΣFθ=0\Sigma F_\theta = 0) the second equation gives ddt(r2θ˙)=0\dfrac{d}{dt}(r^2\dot\theta) = 0, i.e. constant angular momentum h=r2θ˙h = r^2\dot\theta (Kepler's law of areas).

✓ Answer checked by Claude Opus 5.5 (high effort)

All Engineering Mechanics chapter 2 questions →