Physics · Book 3 · Bachelor Year 1

University Physics — Year 1

University Physics — Year 1 · Bachelor Year 1

11Kinematics of a Point

The car on a roller coaster enters the loop at 90km/h90\,\mathrm{km}/\mathrm{h}, slows as it climbs, hangs for an instant at the top, and roars out again; its riders feel crushed into their seats at the bottom and almost weightless at the top. Describing that ride — where the car is, how fast it moves, how its velocity turns and changes — is kinematics, and it needs more than the xx, yy, zz of a straight road: polar coordinates for anything that turns, and a frame that travels with the car itself. This chapter sets up those tools, proves the formulas for velocity and acceleration in each of them, and applies them to the motions that every later chapter will call upon: circular, helical, harmonic, and the motion along any curve.

11.1 Position, velocity, acceleration

Definition 11.1 (Reference frame; position; trajectory)

A reference frame is a rigid body taken as fixed (the laboratory, the Earth, a train), together with a clock. A point particle MM — a body whose size is irrelevant to the motion studied — is located at each instant by its position vector OM(t)\vect{OM}(t) from an origin OO attached to the frame; the curve described by MM is its trajectory. Motion is always motion relative to a frame: the same passenger is at rest in the train and moving in the station.

Definition 11.2 (Velocity and acceleration)

The velocity and acceleration of MM in the frame are

v= ⁣dOM ⁣dt,a= ⁣dv ⁣dt= ⁣d2OM ⁣dt2,\vect v = \frac{\dd\vect{OM}}{\dd t}, \qquad \vect a = \frac{\dd\vect v}{\dd t} = \frac{\dd^2\vect{OM}}{\dd t^2},

derivatives of vector functions: the derivative of a vector is obtained by differentiating its components in a basis that is fixed in the frame. The velocity is tangent to the trajectory and points along the motion; its norm vv is the speed. Units: m/s\mathrm{m}/\mathrm{s}, m/s2\mathrm{m}/\mathrm{s}^{2}.

Proposition 11.3 (Cartesian coordinates)

With a fixed orthonormal basis (ex,ey,ez)(\vect e_x, \vect e_y, \vect e_z) and OM=xex+yey+zez\vect{OM} = x\,\vect e_x + y\,\vect e_y + z\,\vect e_z,

v=x˙ex+y˙ey+z˙ez,a=x¨ex+y¨ey+z¨ez,\vect v = \dot x\,\vect e_x + \dot y\,\vect e_y + \dot z\,\vect e_z, \qquad \vect a = \ddot x\,\vect e_x + \ddot y\,\vect e_y + \ddot z\,\vect e_z,

where the dot denotes  ⁣d/ ⁣dt\dd/\dd t.

Proof. The basis vectors are constant; only the components vary.

Example 11.4 (Projectile)

Launched from OO at speed v0v_0 and angle α\alpha above the horizontal, a ball’s coordinates (dynamics, next chapter) are x=v0cosαtx = v_0\cos\alpha\,t, z=v0sinαt12gt2z = v_0\sin\alpha\,t - \tfrac12 gt^2. Then v=v0cosαex+(v0sinαgt)ez\vect v = v_0\cos\alpha\,\vect e_x + (v_0\sin\alpha - gt)\vect e_z, a=gez\vect a = -g\vect e_z: the acceleration is constant while the velocity turns; at the apex (z˙=0\dot z = 0, t=v0sinα/gt = v_0\sin\alpha/g) the velocity is horizontal and the acceleration perpendicular to it. Eliminating tt: z=xtanαgx2/(2v02cos2α)z = x\tan\alpha - gx^2/(2v_0^2\cos^2\alpha), a parabola.

A projectile’s parabola: the velocity is tangent to the trajectory and turns, the acceleration g is constant. At the apex velocity and acceleration are perpendicular: the speed is momentarily stationary while the direction still changes.
A projectile’s parabola: the velocity is tangent to the trajectory and turns, the acceleration g\vect g is constant. At the apex velocity and acceleration are perpendicular: the speed is momentarily stationary while the direction still changes.

11.2 Cylindrical coordinates

Definition 11.5 (Cylindrical coordinates and basis)

Point MM is located by r0r \geq 0 (distance to the zz axis), the angle θ\theta of its projection on the xyxy plane with ex\vect e_x, and zz: OM=rer+zez\vect{OM} = r\,\vect e_r + z\,\vect e_z, where

er=cosθex+sinθey,eθ=sinθex+cosθey,\vect e_r = \cos\theta\,\vect e_x + \sin\theta\,\vect e_y, \qquad \vect e_\theta = -\sin\theta\,\vect e_x + \cos\theta\,\vect e_y,

and ez\vect e_z form the local basis (er,eθ,ez)(\vect e_r, \vect e_\theta, \vect e_z), orthonormal and direct, which moves with MM. In the plane (zz fixed) these are the polar coordinates (r,θ)(r, \theta).

Lemma 11.6 (Derivatives of the local basis)

 ⁣der ⁣dt=θ˙eθ, ⁣deθ ⁣dt=θ˙er, ⁣dez ⁣dt=0.\frac{\dd\vect e_r}{\dd t} = \dot\theta\,\vect e_\theta, \qquad \frac{\dd\vect e_\theta}{\dd t} = -\dot\theta\,\vect e_r, \qquad \frac{\dd\vect e_z}{\dd t} = \vect 0 .

Proof. Differentiate the components:  ⁣der/ ⁣dt=θ˙(sinθex+cosθey)=θ˙eθ\dd\vect e_r/\dd t = \dot\theta(-\sin\theta\, \vect e_x + \cos\theta\,\vect e_y) = \dot\theta\vect e_\theta, and similarly for eθ\vect e_\theta. A rotating unit vector’s derivative is perpendicular to it, of norm the angular rate.

Theorem 11.7 (Velocity and acceleration in cylindrical coordinates)

v=r˙er+rθ˙eθ+z˙ez,a=(r¨rθ˙2)er+(rθ¨+2r˙θ˙)eθ+z¨ez.\vect v = \dot r\,\vect e_r + r\dot\theta\,\vect e_\theta + \dot z\,\vect e_z, \qquad \vect a = \big(\ddot r - r\dot\theta^2\big)\vect e_r + \big(r\ddot\theta + 2\dot r\dot\theta\big)\vect e_\theta + \ddot z\,\vect e_z .

Proof. Differentiate OM=rer+zez\vect{OM} = r\vect e_r + z\vect e_z with the lemma: v=r˙er+rθ˙eθ+z˙ez\vect v = \dot r\vect e_r + r\dot\theta\vect e_\theta + \dot z\vect e_z. Differentiate again: r¨er+r˙θ˙eθ+r˙θ˙eθ+rθ¨eθrθ˙2er+z¨ez\ddot r\vect e_r + \dot r\dot\theta\vect e_\theta + \dot r\dot\theta\vect e_\theta + r\ddot\theta\vect e_\theta - r\dot\theta^2 \vect e_r + \ddot z\vect e_z; collect.

Polar coordinates: the local basis ( e_r, e_ ) turns with M; the velocity has a radial part r and an orthoradial part r. Here the trajectory (red) spirals outward, so r > 0 and v leans outward from the tangent to the circle.
Polar coordinates: the local basis (er,eθ)(\vect e_r, \vect e_\theta) turns with MM; the velocity has a radial part r˙\dot r and an orthoradial part rθ˙r\dot\theta. Here the trajectory (red) spirals outward, so r˙>0\dot r > 0 and v\vect v leans outward from the tangent to the circle.

Corollary 11.8 (Circular motion)

On a circle of radius RR (r=Rr = R, z=0z = 0), with angular velocity ω=θ˙\omega = \dot\theta:

v=Rωeθ,a=Rω2er+Rω˙eθ=v2Rer+ ⁣dv ⁣dteθ.\vect v = R\omega\,\vect e_\theta, \qquad \vect a = -R\omega^2\,\vect e_r + R\dot\omega\,\vect e_\theta = -\frac{v^2}{R}\,\vect e_r + \frac{\dd v}{\dd t}\,\vect e_\theta .

For uniform circular motion (ω\omega constant) the acceleration is purely centripetal, of norm v2/R=Rω2v^2/R = R\omega^2, although the speed is constant.

Proof. Set r˙=r¨=0\dot r = \ddot r = 0 in the theorem; v=Rωv = R\omega.

Example 11.9 (Two circles)

A car rounds a roundabout of radius 20m20\,\mathrm{m} at 36km/h36\,\mathrm{km}/\mathrm{h} (10m/s10\,\mathrm{m}/\mathrm{s}): a=v2/R=5.0m/s2a = v^2/R = 5.0\,\mathrm{m}/\mathrm{s}^{2}, half a gg, directed toward the center — what the tires must supply. The Moon (R=3.84×108mR = 3.84 \times 10^{8}\,\mathrm{m}, T=27.3dT = 27.3\,\mathrm{d}): ω=2π/T=2.66×106rad/s\omega = 2\pi/T = 2.66 \times 10^{-6}\,\mathrm{rad}/\mathrm{s}, a=Rω2=2.7×103m/s2a = R\omega^2 = 2.7 \times 10^{-3}\,\mathrm{m}/\mathrm{s}^{2}, one 36003600th of gg at the Earth’s surface, at sixty Earth radii — the comparison Newton made (Chapter 16).

11.3 Spherical coordinates

Definition 11.10 (Spherical coordinates)

Point MM is located by its distance r=OMr = OM, the colatitude θ[0,π]\theta \in [0, \pi] between OM\vect{OM} and ez\vect e_z, and the azimuth φ\varphi of its projection on the xyxy plane: OM=rer\vect{OM} = r\,\vect e_r with

er=sinθcosφex+sinθsinφey+cosθez;\vect e_r = \sin\theta\cos\varphi\,\vect e_x + \sin\theta\sin\varphi\,\vect e_y + \cos\theta\,\vect e_z ;

eθ\vect e_\theta (tangent to the meridian, toward increasing θ\theta) and eφ\vect e_\varphi (tangent to the parallel) complete the local orthonormal basis. On the Earth, θ\theta is 9090^\circ minus the latitude and φ\varphi the longitude.

Proposition 11.11 (Velocity in spherical coordinates)

v=r˙er+rθ˙eθ+rsinθφ˙eφ.\vect v = \dot r\,\vect e_r + r\dot\theta\,\vect e_\theta + r\sin\theta\,\dot\varphi\,\vect e_\varphi .

Proof.  ⁣der/ ⁣dt=θ˙eθ+sinθφ˙eφ\dd\vect e_r/\dd t = \dot\theta\,\vect e_\theta + \sin\theta\,\dot\varphi\, \vect e_\varphi: the first term is the rotation in the meridian plane (as in the polar case), the second the rotation about ez\vect e_z at rate φ˙\dot\varphi of a vector whose distance to the axis is sinθ\sin\theta. Then v= ⁣d(rer)/ ⁣dt\vect v = \dd(r\vect e_r)/\dd t. The acceleration is not needed this year.

Spherical coordinates (r, , ) and their local basis: e_r radial, e_ along the meridian (toward the south on a globe), e_ along the parallel (toward the east).
Spherical coordinates (r,θ,φ)(r, \theta, \varphi) and their local basis: er\vect e_r radial, eθ\vect e_\theta along the meridian (toward the south on a globe), eφ\vect e_\varphi along the parallel (toward the east).

11.4 The Frenet frame

Definition 11.12 (Curvilinear abscissa; Frenet basis)

Along a trajectory, the curvilinear abscissa s(t)s(t) is the arc length from a reference point, counted algebraically; v=s˙v = \dot s. At MM, the unit tangent T= ⁣dOM/ ⁣ds\vect T = \dd\vect{OM}/\dd s points along increasing ss; the radius of curvature ρ>0\rho > 0 and the unit normal N\vect N, pointing toward the concave side (the center of curvature), are defined by

 ⁣dT ⁣ds=1ρN.\frac{\dd\vect T}{\dd s} = \frac{1}{\rho}\,\vect N .

(T,N)(\vect T, \vect N) is the Frenet basis; ρ=\rho = \infty on a straight line, ρ=R\rho = R on a circle of radius RR.

Theorem 11.13 (Acceleration in the Frenet basis)

v=vT,a= ⁣dv ⁣dtT+v2ρN.\vect v = v\,\vect T, \qquad \vect a = \frac{\dd v}{\dd t}\,\vect T + \frac{v^2}{\rho}\,\vect N .

The tangential component  ⁣dv/ ⁣dt\dd v/\dd t measures how fast the speed changes; the normal component v2/ρv^2/\rho, always toward the center of curvature, how fast the direction turns. The motion is uniform iff av\vect a \perp \vect v; it is rectilinear iff av\vect a \parallel \vect v.

Proof. v=( ⁣dOM/ ⁣ds)( ⁣ds/ ⁣dt)=vT\vect v = (\dd\vect{OM}/\dd s)(\dd s/\dd t) = v\vect T. Then a=v˙T+v ⁣dT/ ⁣dt=v˙T+v( ⁣dT/ ⁣ds)s˙=v˙T+(v2/ρ)N\vect a = \dot v\vect T + v\,\dd\vect T/\dd t = \dot v\vect T + v(\dd\vect T/\dd s)\dot s = \dot v\vect T + (v^2/\rho)\vect N. That  ⁣dT/ ⁣dsT\dd\vect T/\dd s \perp \vect T follows from TT=1\vect T\cdot\vect T = 1 differentiated.

The Frenet basis at a point of a curve: T along the motion, N toward the center of curvature C. The acceleration splits into a tangential part v T (speeding up or braking) and a normal part (v2/ ) N (turning).
The Frenet basis at a point of a curve: T\vect T along the motion, N\vect N toward the center of curvature CC. The acceleration splits into a tangential part v˙T\dot v\vect T (speeding up or braking) and a normal part (v2/ρ)N(v^2/\rho)\vect N (turning).

Example 11.14 (Braking in a bend)

A car at 90km/h90\,\mathrm{km}/\mathrm{h} (25m/s25\,\mathrm{m}/\mathrm{s}) in a bend of radius 100m100\,\mathrm{m} brakes at 2.0m/s22.0\,\mathrm{m}/\mathrm{s}^{2}: aT=2.0m/s2a_T = -2.0\,\mathrm{m}/\mathrm{s}^{2}, aN=625/100=6.25m/s2a_N = 625/100 = 6.25\,\mathrm{m}/\mathrm{s}^{2}, a=4+39=6.6m/s2a = \sqrt{4 + 39} = 6.6\,\mathrm{m}/\mathrm{s}^{2}. The normal part dominates: a bend is first of all a turning, and the tires’ grip (next chapter) limits aT2+aN2\sqrt{a_T^2 + a_N^2}, which is why one brakes before the bend.

11.5 Standard motions

Proposition 11.15 (Uniformly accelerated rectilinear motion)

On an axis, x¨=a\ddot x = a constant, from x0x_0 and v0v_0: v=v0+atv = v_0 + at, x=x0+v0t+12at2x = x_0 + v_0t + \tfrac12 at^2, and v2v02=2a(xx0)v^2 - v_0^2 = 2a(x - x_0).

Proof. Integrate twice; eliminate tt between the first two relations.

Proposition 11.16 (Helical motion)

r=Rr = R, θ=ωt\theta = \omega t, z=vztz = v_zt (constants RR, ω\omega, vzv_z): the speed v=R2ω2+vz2v = \sqrt{R^2\omega^2 + v_z^2} is constant, the acceleration a=Rω2er\vect a = -R\omega^2\vect e_r is centripetal of constant norm, and the radius of curvature is ρ=v2/a=R(1+vz2/R2ω2)>R\rho = v^2/a = R(1 + v_z^2/R^2\omega^2) > R.

Proof. Theorem 11.7 with r˙=0\dot r = 0, θ¨=0\ddot\theta = 0, z¨=0\ddot z = 0; uniform motion, so a\vect a is purely normal and v2/ρ=Rω2v^2/\rho = R\omega^2.

Proposition 11.17 (Harmonic motion)

x=Acos(ωt+φ)x = A\cos(\omega t + \varphi): x˙=Aωsin(ωt+φ)\dot x = -A\omega\sin(\omega t + \varphi), x¨=ω2x\ddot x = -\omega^2 x. The velocity leads the position by a quarter period and the acceleration is opposite to the position; vmax=Aωv_{\max} = A\omega, amax=Aω2a_{\max} = A\omega^2. This is the projection on a diameter of a uniform circular motion of radius AA and angular velocity ω\omega.

Proof. Differentiate; for the projection, take x=Acosθx = A\cos\theta with θ=ωt+φ\theta = \omega t + \varphi.

Method 11.18 (Choosing coordinates)

  • Straight-line or parabolic motion, constant acceleration: Cartesian.
  • Motion around an axis or a point (circles, spirals, orbits, turntables): cylindrical/polar; the basis moves, so use Theorem 11.7, never naive component differentiation.
  • A given curve (track, bend, loop) when the speed law is known: Frenet, which separates “how fast” from “which way”.

Whatever the choice, v\vect v and a\vect a are frame-dependent vectors, and a result is complete only with the frame named.

11.6 Exercises

Exercise 11.1

A car starts from rest with x(t)=2.0t2x(t) = 2.0\,t^2 (SI units). Velocity and acceleration at t=3.0st = 3.0\,\mathrm{s}; distance covered in the first 5s5\,\mathrm{s}; time to reach 100km/h100\,\mathrm{km}/\mathrm{h}.

Solution

Solution of Exercise 11.1.

v=4.0tv = 4.0t: 12m/s12\,\mathrm{m}/\mathrm{s} at 3.0s3.0\,\mathrm{s}; a=4.0m/s2a = 4.0\,\mathrm{m}/\mathrm{s}^{2}; x(5)=50mx(5) = 50\,\mathrm{m}; 100km/h=27.8m/s100\,\mathrm{km}/\mathrm{h} = 27.8\,\mathrm{m}/\mathrm{s} at t=27.8/4.0=6.9st = 27.8/4.0 = 6.9\,\mathrm{s}.

Exercise 11.2

A point moves in a plane with r=2.0mr = 2.0\,\mathrm{m} and θ=3.0t\theta = 3.0\,t (rad, SI). Give v\vect v and a\vect a in the polar basis, their norms, and the nature of the motion.

Solution

Solution of Exercise 11.2.

r˙=0\dot r = 0, θ˙=3.0rad/s\dot\theta = 3.0\,\mathrm{rad}/\mathrm{s}: v=rθ˙eθ=6.0eθ\vect v = r\dot\theta\,\vect e_\theta = 6.0\,\vect e_\theta (m/s\mathrm{m}/\mathrm{s}); a=rθ˙2er=18er\vect a = -r\dot\theta^2\vect e_r = -18\,\vect e_r (m/s2\mathrm{m}/\mathrm{s}^{2}). Uniform circular motion: constant speed, centripetal acceleration.

Exercise 11.3

A point on the equator (R=6.37×106mR = 6.37 \times 10^{6}\,\mathrm{m}, sidereal day 86164s86\,164\,\mathrm{s}): speed and acceleration in the geocentric frame. Compare the acceleration with gg.

Solution

Solution of Exercise 11.3.

v=2πR/T=2π×6.37×106/86164=465m/sv = 2\pi R/T = 2\pi \times 6.37\times10^6/86164 = 465\,\mathrm{m}/\mathrm{s}; a=v2/R=0.034m/s2a = v^2/R = 0.034\,\mathrm{m}/\mathrm{s}^{2}, g/290g/290.

Exercise 11.4

A ball is thrown with v0=12m/sv_0 = 12\,\mathrm{m}/\mathrm{s} at α=40\alpha = 40^\circ; its coordinates are those of Example 11.4. Find the time to the apex, the maximum height, the range, and the velocity at landing.

Solution

Solution of Exercise 11.4.

v0sinα=7.71m/sv_0\sin\alpha = 7.71\,\mathrm{m}/\mathrm{s}, v0cosα=9.19m/sv_0\cos\alpha = 9.19\,\mathrm{m}/\mathrm{s}. Apex at t=7.71/9.81=0.79st = 7.71/9.81 = 0.79\,\mathrm{s}, height 7.712/(2×9.81)=3.0m7.71^2/(2 \times 9.81) = 3.0\,\mathrm{m}. Range 2×9.19×0.786=14.5m2 \times 9.19 \times 0.786 = 14.5\,\mathrm{m}. Landing: (9.19,7.71)(9.19, -7.71), 12m/s12\,\mathrm{m}/\mathrm{s} at 4040^\circ below the horizontal.

Exercise 11.5 ★★

A cyclist at 10m/s10\,\mathrm{m}/\mathrm{s} enters a bend of radius 25m25\,\mathrm{m} and accelerates at 1.0m/s21.0\,\mathrm{m}/\mathrm{s}^{2}. Give a\vect a in the Frenet basis and its norm; after 5s5\,\mathrm{s} of the same acceleration on the same bend?

Solution

Solution of Exercise 11.5.

aT=1.0m/s2a_T = 1.0\,\mathrm{m}/\mathrm{s}^{2}, aN=102/25=4.0m/s2a_N = 10^2/25 = 4.0\,\mathrm{m}/\mathrm{s}^{2}, a=4.1m/s2a = 4.1\,\mathrm{m}/\mathrm{s}^{2}. After 5s5\,\mathrm{s}: v=15m/sv = 15\,\mathrm{m}/\mathrm{s}, aN=225/25=9.0m/s2a_N = 225/25 = 9.0\,\mathrm{m}/\mathrm{s}^{2}, a=9.1m/s2a = 9.1\,\mathrm{m}/\mathrm{s}^{2}.

Exercise 11.6 ★★

A point follows the spiral r=bθr = b\theta, θ=ωt\theta = \omega t (bb, ω\omega constants). Compute v\vect v, the speed, and a\vect a in the polar basis. Where does the 2r˙θ˙2\dot r\dot\theta term come from?

Solution

Solution of Exercise 11.6.

r=bωtr = b\omega t, r˙=bω\dot r = b\omega, r¨=0\ddot r = 0, θ˙=ω\dot\theta = \omega: v=bωer+bω2teθ\vect v = b\omega\,\vect e_r + b\omega^2 t\,\vect e_\theta, v=bω1+ω2t2v = b\omega \sqrt{1 + \omega^2t^2}; a=bω3ter+2bω2eθ\vect a = -b\omega^3 t\,\vect e_r + 2b\omega^2\, \vect e_\theta. The 2r˙θ˙2\dot r\dot\theta term has two equal halves: the radial velocity’s direction turns at rate θ˙\dot\theta (giving r˙θ˙eθ\dot r\dot\theta\,\vect e_\theta), and moving outward increases the orthoradial speed rθ˙r\dot\theta (another r˙θ˙\dot r\dot\theta).

Exercise 11.7 ★★

Helix: R=2.0mR = 2.0\,\mathrm{m}, ω=1.0rad/s\omega = 1.0\,\mathrm{rad}/\mathrm{s}, vz=0.50m/sv_z = 0.50\,\mathrm{m}/\mathrm{s}. Speed, acceleration, pitch of the helix, radius of curvature.

Solution

Solution of Exercise 11.7.

v=(2.0×1.0)2+0.52=2.1m/sv = \sqrt{(2.0 \times 1.0)^2 + 0.5^2} = 2.1\,\mathrm{m}/\mathrm{s}; a=Rω2=2.0m/s2a = R\omega^2 = 2.0\,\mathrm{m}/\mathrm{s}^{2} toward the axis; pitch vz×2π/ω=3.1mv_z \times 2\pi/\omega = 3.1\,\mathrm{m}; ρ=v2/a=4.25/2.0=2.1m>R\rho = v^2/a = 4.25/2.0 = 2.1\,\mathrm{m} > R.

Exercise 11.8 ★★

A piston moves as x=0.10cos(10t)x = 0.10\cos(10t) (SI). Give vmaxv_{\max}, amaxa_{\max}, the phase relations between xx, vv, aa, and the positions where v\abs v and a\abs a are largest.

Solution

Solution of Exercise 11.8.

vmax=Aω=1.0m/sv_{\max} = A\omega = 1.0\,\mathrm{m}/\mathrm{s}; amax=Aω2=10m/s2a_{\max} = A\omega^2 = 10\,\mathrm{m}/\mathrm{s}^{2}; vv leads xx by a quarter period, a=ω2xa = -\omega^2x is opposite to xx. v\abs v is largest at x=0x = 0, a\abs a at the extremes x=±Ax = \pm A.

Exercise 11.9 ★★

Starting from er=cosθex+sinθey\vect e_r = \cos\theta\,\vect e_x + \sin\theta\,\vect e_y, derive  ⁣der/ ⁣dt\dd\vect e_r/\dd t and  ⁣deθ/ ⁣dt\dd\vect e_\theta/\dd t, and then the polar velocity and acceleration of Theorem 11.7.

Solution

Solution of Exercise 11.9.

e˙r=θ˙(sinθex+cosθey)=θ˙eθ\dot{\vect e}_r = \dot\theta(-\sin\theta\,\vect e_x + \cos\theta\,\vect e_y) = \dot\theta\,\vect e_\theta; e˙θ=θ˙(cosθexsinθey)=θ˙er\dot{\vect e}_\theta = \dot\theta(-\cos\theta\, \vect e_x - \sin\theta\,\vect e_y) = -\dot\theta\,\vect e_r. Then v=r˙er+rθ˙eθ\vect v = \dot r\vect e_r + r\dot\theta\vect e_\theta, and differentiating once more with the product rule gives the acceleration of Theorem 11.7.

Exercise 11.10 ★★★

For the projectile of Example 11.4, find the radius of curvature of the trajectory at the apex and at the launch point (use the normal component of g\vect g). Which is smaller, and why?

Solution

Solution of Exercise 11.10.

Apex: v=v0cosαv = v_0\cos\alpha, aN=ga_N = g: ρ=v02cos2α/g\rho = v_0^2\cos^2\alpha/g. Launch: v=v0v = v_0, aN=gcosαa_N = g\cos\alpha: ρ=v02/(gcosα)\rho = v_0^2/(g\cos\alpha). The apex radius is smaller by cos3α\cos^3\alpha: the parabola bends most where it is slowest and where all of g\vect g is normal.

Exercise 11.11 ★★★

A wheel of radius RR rolls without slipping at speed vv; a point of its rim has coordinates x=vtRsin(vt/R)x = vt - R\sin(vt/R), y=RRcos(vt/R)y = R - R\cos(vt/R) (a cycloid). Compute its velocity and acceleration; show that when it touches the ground its velocity vanishes and its acceleration is v2/Rv^2/R upward; find its speed at the top.

Solution

Solution of Exercise 11.11.

x˙=vvcos(vt/R)\dot x = v - v\cos(vt/R), y˙=vsin(vt/R)\dot y = v\sin(vt/R); x¨=(v2/R)sin(vt/R)\ddot x = (v^2/R) \sin(vt/R), y¨=(v2/R)cos(vt/R)\ddot y = (v^2/R)\cos(vt/R). At the ground (vt/R=2πnvt/R = 2\pi n): x˙=y˙=0\dot x = \dot y = 0 and a=(0,v2/R)\vect a = (0, v^2/R), upward. At the top (vt/R=πvt/R = \pi): x˙=2v\dot x = 2v, y˙=0\dot y = 0: speed 2v2v.

Exercise 11.12 ★★★

A person walks outward along a radius of a turntable turning at constant ω\omega, at constant speed uu relative to the turntable: r=utr = ut, θ=ωt\theta = \omega t. Compute a\vect a in the polar basis, identify the two terms, and evaluate them for u=1.0m/su = 1.0\,\mathrm{m}/\mathrm{s}, ω=1.0rad/s\omega = 1.0\,\mathrm{rad}/\mathrm{s} at t=2.0st = 2.0\,\mathrm{s}. Which term has no counterpart for a person walking on the ground?

Solution

Solution of Exercise 11.12.

r¨=0\ddot r = 0, r˙=u\dot r = u, θ˙=ω\dot\theta = \omega: a=utω2er+2uωeθ\vect a = -ut\omega^2\, \vect e_r + 2u\omega\,\vect e_\theta. At t=2.0st = 2.0\,\mathrm{s}: 2.0er+2.0eθ-2.0\,\vect e_r + 2.0\,\vect e_\theta (m/s2\mathrm{m}/\mathrm{s}^{2}). The first is the centripetal term of the rotation; the second, 2r˙θ˙2\dot r\dot\theta, exists only because the radial direction itself rotates — on the ground, walking straight at constant speed gives no acceleration at all.

A vertical loop (Yomiuriland, Tokyo): a teardrop rather than a circle, so that the curvature is largest at the top where the speed is least — the geometry of the weekend problem. Photograph: Jeremy Thompson, CC BY 2.0.
A vertical loop (Yomiuriland, Tokyo): a teardrop rather than a circle, so that the curvature is largest at the top where the speed is least — the geometry of the weekend problem. Photograph: Jeremy Thompson, CC BY 2.0.

11.7 Problem: The roller-coaster loop

Problem 11.1

Weekend problem — a car enters a vertical loop at ninety kilometers per hour: where it slows, where its acceleration points, how many gg the riders feel, and why modern loops are not circles

A car, treated as a point MM, runs on a vertical circular loop of radius R=10mR = 10\,\mathrm{m}, center CC. Its position is given by the angle θ\theta between CM\vect{CM} and the downward vertical (θ=0\theta = 0 at the bottom, π\pi at the top). Friction is neglected, and the speed law (derived in Chapter 13) is

v2=v022gR(1cosθ),v^2 = v_0^2 - 2gR(1 - \cos\theta),

with v0=25m/sv_0 = 25\,\mathrm{m}/\mathrm{s} the speed at the bottom; g=9.81m/s2g = 9.81\,\mathrm{m}/\mathrm{s}^{2}.

Part I — Kinematics on the circle.

  1. In polar coordinates centered at CC (with er\vect e_r from CC to MM), write v\vect v and a\vect a for motion on the circle.
  2. Identify the Frenet vectors T\vect T and N\vect N in terms of er\vect e_r and eθ\vect e_\theta, and the radius of curvature.
  3. Compute the speed at the top, and at the side points θ=π/2\theta = \pi/2 and 3π/23\pi/2.
  4. Differentiate the speed law with respect to time to show that the tangential acceleration is aT=gsinθa_T = -g\sin\theta. Interpret its sign on the way up and on the way down.
  5. Express the normal acceleration aN(θ)a_N(\theta) and compute it at the bottom, the sides and the top.
  6. Give the norm of a\vect a at the four points and the angle it makes with the vertical at the top.
  7. At which points is a\vect a perpendicular to v\vect v? Parallel?

Part II — Angular rates and timing.

  1. Express θ˙\dot\theta as a function of θ\theta and compute it at the bottom and the top.
  2. Show that θ¨=(g/R)sinθ\ddot\theta = -(g/R)\sin\theta (the equation of a pendulum) and comment.
  3. For comparison, compute the period of small oscillations of a simple pendulum of length RR (Example 1.8 gave its form; k=2πk = 2\pi).
  4. Estimate the time to go round the loop, using the average of the speeds at the four reference points.
  5. The minimum speed at the top for the car to stay on the track (next chapter) is gR\sqrt{gR}. Is it satisfied? What minimum v0v_0 would be needed?

Part III — What the riders feel. The apparent weight per unit mass felt by a rider is ag\vect a - \vect g (admitted here, derived in Chapter 12); its norm in units of gg is the “gg-load”.

  1. Compute the gg-load at the bottom.
  2. Compute it at the top, and say which way the rider is pressed (seat or restraint).
  3. Compute it at the side points.
  4. Riders tolerate about 4g4g briefly. Does this loop pass? Where is the problem?
  5. Show that, for a circular loop entered just fast enough to clear the top (zero apparent weight there), the bottom gg-load is necessarily 6g6g, whatever RR.

Part IV — The clothoid loop. Modern loops are “teardrops”: the radius of curvature is large at the bottom and small at the top.

  1. Using the Frenet form of a\vect a, explain why varying ρ\rho along the track changes aNa_N without changing the speed law (which depends only on height).
  2. Choose ρbottom\rho_{\text{bottom}} so that the gg-load at the bottom is 3g3g with v0=25m/sv_0 = 25\,\mathrm{m}/\mathrm{s}.
  3. At the top, the height is still 2R=20m2R = 20\,\mathrm{m} above the bottom. Choose ρtop\rho_{\text{top}} so that the gg-load there is 1.5g1.5g.
  4. A clothoid has curvature proportional to arc length, 1/ρ=s/A21/\rho = s/A^2. Along such an entry, with the speed nearly constant, how does aNa_N grow with time, and why is that gentler on the neck than a circle (where aNa_N jumps at the entry)?
  5. Sketch the resulting loop shape qualitatively and summarize in two sentences why it replaced the circle.

Part V — Seen from the ground. A camera at ground level, 50m50\,\mathrm{m} from the loop’s center in its plane, follows the car.

  1. When the car is at the top, moving horizontally at 15m/s15\,\mathrm{m}/\mathrm{s}, at what angular rate (rad/s) must the camera turn? (Polar coordinates from the camera.)
  2. Why is a camera that turns at constant rate a poor tracker of uniform circular motion?
  3. Summarize the chapter’s lesson from the loop: which coordinate system answered which question.
Solution

Solution of Problem 11.1.

1. v=Rθ˙eθ\vect v = R\dot\theta\,\vect e_\theta; a=Rθ˙2er+Rθ¨eθ\vect a = -R\dot\theta^2 \,\vect e_r + R\ddot\theta\,\vect e_\theta.

2. T=eθ\vect T = \vect e_\theta (motion with θ\theta increasing), N=er\vect N = -\vect e_r (toward CC), ρ=R\rho = R.

3. Top: v2=625392=233v^2 = 625 - 392 = 233, v=15.3m/sv = 15.3\,\mathrm{m}/\mathrm{s}. Sides: 625196=429625 - 196 = 429, v=20.7m/sv = 20.7\,\mathrm{m}/\mathrm{s}.

4. 2vv˙=2gRsinθθ˙2v\dot v = -2gR\sin\theta\,\dot\theta and v=Rθ˙v = R\dot\theta: v˙=gsinθ\dot v = -g\sin\theta. Negative for 0<θ<π0 < \theta < \pi (slowing on the way up), positive on the way down.

5. aN=v2/R=v02/R2g(1cosθ)a_N = v^2/R = v_0^2/R - 2g(1 - \cos\theta): bottom 62.5m/s262.5\,\mathrm{m}/\mathrm{s}^{2}; sides 62.519.6=42.9m/s262.5 - 19.6 = 42.9\,\mathrm{m}/\mathrm{s}^{2}; top 62.539.2=23.3m/s262.5 - 39.2 = 23.3\,\mathrm{m}/\mathrm{s}^{2}.

6. Bottom: 62.5m/s262.5\,\mathrm{m}/\mathrm{s}^{2} (no tangential part); sides: 42.92+9.812=44.0m/s2\sqrt{42.9^2 + 9.81^2} = 44.0\,\mathrm{m}/\mathrm{s}^{2}; top: 23.3m/s223.3\,\mathrm{m}/\mathrm{s}^{2}, pointing straight down toward CC: angle 00 with the vertical.

7. Perpendicular at the bottom and top (aT=0a_T = 0); never parallel (aN>0a_N > 0 everywhere).

8. θ˙=v/R=v022gR(1cosθ)/R\dot\theta = v/R = \sqrt{v_0^2 - 2gR(1 - \cos\theta)}/R: bottom 2.50rad/s2.50\,\mathrm{rad}/\mathrm{s}, top 1.53rad/s1.53\,\mathrm{rad}/\mathrm{s}.

9. θ¨=v˙/R=(g/R)sinθ\ddot\theta = \dot v/R = -(g/R)\sin\theta: the equation of a simple pendulum of length RR — the car on its track is a pendulum bob that goes over the top.

10. 2πR/g=2π10/9.81=6.3s2\pi\sqrt{R/g} = 2\pi\sqrt{10/9.81} = 6.3\,\mathrm{s}.

11. Mean of 2525, 20.720.7, 15.315.3, 20.720.7: about 20m/s20\,\mathrm{m}/\mathrm{s}; length 2πR=63m2\pi R = 63\,\mathrm{m}: roughly 3s3\,\mathrm{s}.

12. gR=9.9m/s<15.3\sqrt{gR} = 9.9\,\mathrm{m}/\mathrm{s} < 15.3: yes. Minimum: v02gR+4gR=5gR=490v_0^2 \geq gR + 4gR = 5gR = 490, v022.1m/sv_0 \geq 22.1\,\mathrm{m}/\mathrm{s}.

13. Bottom: a=62.5\vect a = 62.5 upward, g\vect g downward: ag=62.5+9.8=72.3m/s2=7.4g\abs{\vect a - \vect g} = 62.5 + 9.8 = 72.3\,\mathrm{m}/\mathrm{s}^{2} = 7.4g.

14. Top: both downward, 23.39.8=13.5m/s2=1.4g23.3 - 9.8 = 13.5\,\mathrm{m}/\mathrm{s}^{2} = 1.4g, pressing the rider into the seat (toward the center, i.e. upward for the inverted rider).

15. Sides: a=42.9\vect a = 42.9 horizontal toward CC plus 9.89.8 downward (tangential); ag\vect a - \vect g is 42.942.9 horizontal: 4.4g4.4g sideways, toward the center.

16. Fails: 7.4g7.4g at the bottom (the top and sides are fine).

17. Zero apparent weight at the top: vtop2=gRv_{\text{top}}^2 = gR; then v02=gR+4gR=5gRv_0^2 = gR + 4gR = 5gR, aN=5ga_N = 5g at the bottom and the load is 5g+g=6g5g + g = 6g, independent of RR.

18. aN=v2/ρa_N = v^2/\rho: vv is fixed by the height (energy), ρ\rho by the track’s geometry; a different ρ\rho at the same height changes aNa_N alone.

19. aN+g=3ga_N + g = 3g: aN=2ga_N = 2g, ρ=v02/2g=625/19.6=32m\rho = v_0^2/2g = 625/19.6 = 32\,\mathrm{m}.

20. vtop=15.3m/sv_{\text{top}} = 15.3\,\mathrm{m}/\mathrm{s}; aNg=1.5ga_N - g = 1.5g: aN=24.5m/s2a_N = 24.5\,\mathrm{m}/\mathrm{s}^{2}, ρ=233/24.5=9.5m\rho = 233/24.5 = 9.5\,\mathrm{m}.

21. aN=v2/ρ=v2s/A2=v3t/A2a_N = v^2/\rho = v^2s/A^2 = v^3t/A^2: it grows linearly from zero — a constant rate of change of acceleration — instead of jumping from 00 to v2/Rv^2/R at the entry of a circle, which the neck feels as a blow.

22. A teardrop: wide and gently curved at the bottom where the car is fast, tight at the top where it is slow. It keeps the load near 3g3g throughout and brings it on gradually.

23. Line of sight: horizontal distance 50m50\,\mathrm{m}, height 20m20\,\mathrm{m}: r=53.9mr = 53.9\,\mathrm{m}, elevation β=21.8\beta = 21.8^\circ. The horizontal velocity’s transverse component is vsinβ=15×0.371=5.6m/sv\sin\beta = 15 \times 0.371 = 5.6\,\mathrm{m}/\mathrm{s}; θ˙=5.6/53.9=0.10rad/s\dot\theta = 5.6/53.9 = 0.10\,\mathrm{rad}/\mathrm{s}.

24. Seen from an off-center point the angular rate of the line of sight is not constant (fast when the car is near, slow when far): a constant-rate camera drifts off the car.

25. Polar coordinates at CC for velocity and acceleration on the circle; the Frenet split for “speeding up” versus “turning” and for the clothoid; polar coordinates at the camera for the tracking rate; energy (next chapters) for the speed law.

Terms defined in this chapter

See all 393 terms in the glossary