An interesting trajectory

A particle describes a path (see the figure below) which in polar coordinates is given by the equation r 2 = R 2 cos ( 2 θ ) . r^{2}= R^{2}\cos(2\theta). It turns out that such trajectory is possible when the particle moves under the influence of a central force of the form F ( r ) = C r n F(r)=\frac{C}{r^{n}} where C C is a constant, r r is the distance to the origin O and n n is an integer. Determine n n .

Note that a central force is always directed toward a fixed point (point O in this case).

Details and assumptions

  • Consider only one half of the diagram, i.e. the particle travels around the left lobe or the right lobe, but not both.


The answer is 7.

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4 solutions

Derek Khu
Aug 27, 2013

We can see this as a classical central-force problem, and thus apply the Binet's equation to solve this problem. Before we begin solving the problem, a brief overview of the derivation of the equation is as follows: we know that particles moving under a central force experience no change in angular momentum, since the central force only acts in the radial component of the acceleration of the particle [for the full mathematical proof, look here ]. So we can let h h be the specific angular momentum of the particle (which is the angular momentum of the particle divided by its mass m m ), where h h is a constant. Now, if we let u = 1 r u = \frac{1}{r} be the reciprocal of the distance from the origin, then we can write the central force in terms of u u using Binet's formula: F ( u ) = m h 2 u 2 ( d 2 u d θ 2 + u ) F(u) = -mh^2u^2\left(\dfrac{\mathrm{d}^{2}u}{\mathrm{d}\theta^2}+u\right) [for the full mathematical proof, look here ].

So first, we need to determine what d 2 u d θ 2 \dfrac{\mathrm{d}^{2}u}{\mathrm{d}\theta^2} is.

r 2 = R 2 cos ( 2 θ ) 1 u 2 = R 2 cos ( 2 θ ) d d θ ( 1 u 2 ) = d d θ [ R 2 cos ( 2 θ ) ] 1 u 3 d u d θ = R 2 sin ( 2 θ ) d u d θ = u 3 R 2 sin ( 2 θ ) d 2 u d θ 2 = R 2 u 3 [ 2 cos ( 2 θ ) ] + R 2 sin ( 2 θ ) ( 3 u 2 d u d θ ) = 2 u 3 [ R 2 cos ( 2 θ ) ] + 3 u 5 R 2 sin ( 2 θ ) ( 1 u 3 d u d θ ) = 2 u 3 ( 1 u 2 ) + 3 u 5 R 2 sin ( 2 θ ) [ R 2 sin ( 2 θ ) ] = 2 u + 3 u 5 R 4 sin 2 ( 2 θ ) = 2 u + 3 u 5 R 4 [ 1 cos 2 ( 2 θ ) ] = 2 u + 3 u 5 R 4 3 u 5 R 4 cos 2 ( 2 θ ) = 2 u + 3 u 5 R 4 3 u 5 [ R 2 cos ( 2 θ ) ] 2 = 2 u + 3 u 5 R 4 3 u 5 ( 1 u 2 ) 2 = 2 u + 3 u 5 R 4 3 u = 3 u 5 R 4 u r^2 = R^2 \cos (2\theta) \\ \dfrac{1}{u^2} = R^2 \cos (2\theta) \\ \dfrac{\mathrm{d}}{\mathrm{d}\theta}(\dfrac{1}{u^2}) = \dfrac{\mathrm{d}}{\mathrm{d}\theta}[R^2 \cos (2\theta)] \\ \dfrac{1}{u^3}\dfrac{\mathrm{d}u}{\mathrm{d}\theta} = R^2 \sin (2\theta) \\ \dfrac{\mathrm{d}u}{\mathrm{d}\theta} = u^3 R^2 \sin (2\theta) \\ \begin{aligned} \dfrac{\mathrm{d}^{2}u}{\mathrm{d}\theta^2} &= R^2u^3[2 \cos (2\theta)] + R^2 \sin (2\theta) (3u^2 \dfrac{\mathrm{d}u}{\mathrm{d}\theta}) \\ &= 2u^3[R^2 \cos (2\theta)]+ 3u^5R^2 \sin (2\theta) (\dfrac{1}{u^3} \dfrac{\mathrm{d}u}{\mathrm{d}\theta}) \\ &= 2u^3(\dfrac{1}{u^2})+ 3u^5R^2 \sin (2\theta) [R^2 \sin (2\theta)] \\ &= 2u + 3u^5R^4 \sin^2 (2\theta) \\ &= 2u + 3u^5R^4 [1 - \cos^2 (2\theta)] \\ &= 2u + 3u^5R^4 - 3u^5R^4 \cos^2 (2\theta) \\ &= 2u + 3u^5R^4 - 3u^5[R^2 \cos (2\theta)]^2 \\ &= 2u + 3u^5R^4 - 3u^5(\dfrac{1}{u^2})^2 \\ &= 2u + 3u^5R^4 - 3u \\ &= 3u^5R^4 - u \end{aligned}

So now we substitute this back into the Binet's equation to obtain

F ( u ) = m h 2 u 2 ( d 2 u d θ 2 + u ) = m h 2 u 2 ( 3 u 5 R 4 u + u ) = m h 2 u 2 ( 3 u 5 R 4 ) = 3 R 4 m h 2 u 7 . \begin{aligned} F(u) &= -mh^2u^2\left(\dfrac{\mathrm{d}^{2}u}{\mathrm{d}\theta^2}+u\right) \\ &= -mh^2u^2(3u^5R^4 - u + u) \\ &= -mh^2u^2(3u^5R^4) \\ &= -3R^4mh^2u^7 . \end{aligned}

Since r = 1 u r = \dfrac{1}{u} , then we can substitute this back into the expression above to get

F ( r ) = F ( 1 u ) = 3 R 4 m h 2 ( 1 u ) 7 = 3 R 4 m h 2 u 7 = C u 7 , \begin{aligned} F(r) &= F(\dfrac{1}{u}) \\ &= -3R^4mh^2(\dfrac{1}{u})^7 \\ &= \dfrac{-3R^4mh^2}{u^7} \\ &= \dfrac{C}{u^7} , \end{aligned} where C = 3 R 4 m h 2 C = -3R^4mh^2 is a constant.

Therefore, n = 7 n = 7 .

Mark Hennings
Aug 27, 2013

In planar polar coordinates, the radial and transverse components of acceleration are r ¨ r θ ˙ 2 \ddot{r} - r\dot\theta^2 and r θ ¨ + 2 r r ˙ θ ˙ = 1 r d d t ( r 2 θ ˙ ) r\ddot\theta + 2r\dot{r}\dot\theta = \tfrac{1}{r}\tfrac{d}{dt}(r^2\dot\theta) . Thus, for a particle of mass m m in an attractive central field of magnitude F ( r ) = C r n F(r)=\tfrac{C}{r^n} , we have r ¨ r θ ˙ 2 = C m r n h = r 2 θ ˙ \ddot{r} - r\dot\theta^2 = -\tfrac{C}{m}r^{-n} \qquad \qquad h \; = \; r^2\dot\theta where h h is constant, the angular momentum per unit mass.

If we change variables, and consider u = r 1 u = r^{-1} , then r ˙ = u 2 d u d θ θ ˙ = h d u d θ r ¨ = h d 2 u d θ 2 θ ˙ = h 2 u 2 d 2 u d θ 2 \begin{array}{rcl} \dot{r} & = & -u^{-2}\frac{du}{d\theta}\dot\theta \; = \; -h\frac{du}{d\theta} \\ \ddot{r} & = & -h\frac{d^2u}{d\theta^2}\dot\theta \; = \; -h^2u^2\frac{d^2u}{d\theta^2} \end{array} so that the differential equation becomes h 2 u 2 d 2 u d θ 2 h 2 u 3 = C m u n d 2 u d θ 2 + u = C m h 2 u n 2 \begin{array}{rcl} -h^2u^2\frac{d^2u}{d\theta^2} - h^2u^3 & = & -\tfrac{C}{m}u^n \\ \frac{d^2u}{d\theta^2} + u & = & \tfrac{C}{mh^2}u^{n-2} \end{array} The trajectory r 2 = R 2 cos 2 θ r^2 = R^2\cos2\theta leads to u = R 1 ( sec 2 θ ) 1 2 d u d θ = R 1 1 2 ( sec 2 θ ) 1 2 × 2 sec 2 θ tan 2 θ = R 1 ( sec 2 θ ) 1 2 tan 2 θ d 2 u d θ 2 = R 1 ( sec 2 θ ) 1 2 tan 2 2 θ + 2 R 1 ( sec 2 θ ) 1 2 sec 2 2 θ = R 1 [ tan 2 2 θ + 2 sec 2 2 θ ] ( sec 2 θ ) 1 2 d 2 u d θ 2 + u = R 1 [ tan 2 2 θ + 1 + 2 sec 2 2 θ ] ( sec 2 θ ) 1 2 = 3 R ( sec 2 θ ) 5 2 = 3 R 4 u 5 \begin{array}{rcl} u & = & R^{-1}(\sec2\theta)^{\frac12} \\ \frac{du}{d\theta} & = & R^{-1}\tfrac{1}{2}(\sec2\theta)^{-\frac12} \times2\sec2\theta\tan2\theta \\ & = & R^{-1}(\sec2\theta)^{\frac12}\tan2\theta \\ \frac{d^2u}{d\theta^2} & = & R^{-1}(\sec2\theta)^{\frac12}\tan^22\theta + 2R^{-1}(\sec2\theta)^{\frac12}\sec^22\theta \\ & = & R^{-1}\big[\tan^22\theta + 2\sec^22\theta\big](\sec2\theta)^{\frac12} \\ \frac{d^2u}{d\theta^2} + u & = & R^{-1}\big[\tan^22\theta + 1 + 2\sec^22\theta\big](\sec2\theta)^{\frac12} \\ & = & \tfrac{3}{R}(\sec2\theta)^{\frac52} \; = \; 3R^4u^5 \end{array} and so this trajectory is possible provided that n = 7 n=7 .

Suppose that the particle did try to follow this path, and assume that θ = 0 \theta=0 when t = 0 t=0 . Since R 2 cos 2 θ θ ˙ = h R^2\cos2\theta\, \dot\theta = h , we deduce that sin 2 θ = 2 h t R 2 0 t R 2 2 h \sin2\theta \; = \; \tfrac{2ht}{R^2} \qquad \qquad 0 \le t \le \tfrac{R^2}{2h} and hence r = ( R 4 4 h 2 t 2 ) 1 4 0 t R 2 2 h r \; = \; \big(R^4 - 4h^2t^2\big)^{\frac14} \qquad \qquad 0 \le t \le \tfrac{R^2}{2h} Chasing the formulae, the speed of the particle at any point is v = R 2 h ( R 4 4 h 2 t 2 ) 3 4 v \; = \; R^2h\big(R^4 - 4h^2t^2\big)^{-\frac34} Thus, in a finite time R 2 2 h \tfrac{R^2}{2h} the particle attains infinite speed and reaches the origin, where it presumably has a fairly satisfying collision with the source of the central force. It strikes me as unlikely that the particle will survive to make it into the left-hand half of the curve!

Mark Hennings - 7 years, 9 months ago
Ganesh Sundaram
Aug 26, 2013

Reference: See for example David Morin's book on Classical Mechanics.

First note that the force law F ( r ) = C / r n , C < 0 , F(r) = C/r^n , \ C < 0, implies that the potential is V ( r ) = C n r n 1 B r n 1 such that F ( r ) = d V d r V ( r ) . V(r) = - \frac{C}{nr^{n-1}} \equiv \frac{B}{r^{n-1}} \ \text{such that } F(r) = -\frac{dV}{dr} \equiv - V'(r).

For central forces, acceleration is only along the radial direction. The tangential part is zero. The radial and tangential accelerations of a point mass in polar coordinates are a r = r ¨ r θ ˙ 2 ; a θ = 2 r ˙ θ ˙ + r θ ¨ = 0. a_r = \ddot{r} - r \dot{\theta}^2; \qquad a_\theta = 2\dot{r}\dot{\theta} + r\ddot{\theta} = 0. The second equation results in the conservation of angular momentum L L and it allows us to express angular velocity in terms of L L : L = m r 2 θ ˙ = Const. θ ˙ = L m r 2 L = mr^2\dot \theta = \text{Const.} \quad \Rightarrow \dot{\theta} = \frac{L}{mr^2} The Newton's law can now be expressed as m a r = m r ¨ L m r 3 = F ( r ) = V ( r ) . m a_r = m \ddot{r} - \frac{L}{mr^3} = F(r) = - V'(r). This equation can be integrated once (after multiplication with r ˙ \dot{r} ) to yield conservation energy equation: 1 2 m r ˙ 2 + L 2 m r 2 + V ( r ) = E . \frac{1}{2} m \dot{r}^2 + \frac{L}{2mr^2} + V(r) = E.

Noting that r ˙ = d r d θ θ ˙ = d r d θ L m r 2 , \dot{r} = \frac{dr}{d\theta} \dot{\theta} = \frac{dr}{d\theta} \frac{L}{mr^2}, the conservation energy equation can be transformed into ( 1 r 2 d r d θ ) 2 + 1 r 2 = 2 m E L 2 2 m V ( r ) L 2 . \left(\frac{1}{r^2} \frac{dr}{d\theta}\right)^2 + \frac{1}{r^2}= \frac{2mE}{L^2} - \frac{2mV(r)}{L^2}. Given r 2 ( θ ) = R 2 cos ( 2 θ ) r^2(\theta) = R^2 \cos(2\theta) , and noting that r d r d θ = R 2 sin ( 2 θ ) , r \frac{dr}{d\theta} = - R^2 \sin (2\theta), and substituting this into the last differential equation, we get R 4 r 6 = 2 m E L 2 + 2 m V ( r ) L 2 . \frac{R^4}{r^6} = \frac{2mE}{L^2} + \frac{2mV(r)}{L^2}. Comparing the equations, it is evident that E = 0 , and n = 7. E = 0, \text{ and } n = 7.

A typo: In the first equation, the expression for V ( r ) V(r) should not contain a " - " sign: V ( r ) = C n r n 1 B r n 1 . . . and so on V(r) = \frac{C}{nr^{n-1}} \equiv \frac{B}{r^{n-1}} ... \text{ and so on } Another typo: In the conservation of energy equation and the equation above, there should have been L 2 L^2 instead of L L . Here are corrected equations:

The Newton's law can now be expressed as m a r = m r ¨ L 2 m r 3 = F ( r ) = V ( r ) . m a_r = m \ddot{r} - \frac{L^2}{mr^3} = F(r) = - V'(r). This equation can be integrated once (after multiplication with r ˙ \dot{r} ) to yield conservation energy equation: 1 2 m r ˙ 2 + L 2 2 m r 2 + V ( r ) = E . \frac{1}{2} m \dot{r}^2 + \frac{L^2}{2mr^2} + V(r) = E.

Ganesh Sundaram - 7 years, 9 months ago
Akul Agrawal
Oct 13, 2015

Simplest solution from elementry concepts

I think it is motivated by the above solutions but presented in a basic way

Aditya Kumar - 5 years, 7 months ago

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Well, talking frankly... I didn't get most of the above solutions for I don't know anything about Binet's equation.

And yes, it was my motive to present solution in a basic way so that everyone can understand it.

Akul Agrawal - 5 years, 7 months ago

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