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Problem Irodov 1.176

Three identical discs of equal mass, AA, BB and CC, lie on a smooth (frictionless) horizontal plane. Discs BB and CC are at rest, their centers a distance η\eta times each disc’s diameter dd apart. Disc AA, set moving with velocity v\vect v along the perpendicular bisector of the line joining BB’s and CC’s centers, strikes both simultaneously in one elastic collision. Find disc AA’s velocity v′v' after the collision, as a function of vv and η\eta, and determine the ranges of η\eta for which AA recoils, stops, or continues moving forward.

Redrawn from the book's figure: the three identical discs at the instant of simultaneous contact, disc A arriving along v on the perpendicular bisector of BC and touching B and C together.

Redrawn from the book’s figure: the three identical discs at the instant of simultaneous contact, disc AA arriving along v\vect v on the perpendicular bisector of BCBC and touching BB and CC together.

Given
  • vv
  • η\eta (with 1≤η≤21\le\eta\le2: η≥1\eta\ge1 since BB and CC must not overlap, η≤2\eta\le2 since sin⁡θ≤1\sin\theta\le1)
Find
v′v' (magnitude and sign along v\vect v); the ranges of η\eta for recoil, stop, continue

Solution

Step 1The contact angle from the geometry
The same instant as a triangle of centers: isosceles, with AB=AC=d and base BC=η d. The dashed axis of symmetry, along which v points, bisects the apex angle at A and meets BC square, fixing the half-angle θ.

The same instant as a triangle of centers: isosceles, with AB=AC=dAB=AC=d and base BC=ηdBC=\eta d. The dashed axis of symmetry, along which v\vect v points, bisects the apex angle at AA and meets BCBC square, fixing the half-angle θ\theta.

Touching discs have centers one diameter apart, which is what fixes AB=AC=dAB=AC=d. Reading the right triangle above (the altitude from AA bisects the isosceles apex and lands at BCBC’s midpoint) gives sin⁡θ\sin\theta directly in terms of η\eta, and the identity cos⁡2θ=1−sin⁡2θ\cos^2\theta=1-\sin^2\theta converts it to the form the momentum and energy equations below will need.

sin⁡θ=η2cos⁡2θ=1−η24(1) \begin{aligned} \sin\theta &= \frac{\eta}{2} \\ \cos^2\theta &= 1-\frac{\eta^2}{4} \end{aligned} \tag{1}
Step 2Momentum and energy along the line of motion
The outgoing velocities this step establishes: B leaves at the angle θ above the axis and C at θ below it, at the same speed by symmetry, while A stays on the axis.

The outgoing velocities this step establishes: BB leaves at the angle θ\theta above the axis and CC at θ\theta below it, at the same speed by symmetry, while AA stays on the axis.

That same symmetry makes the two struck discs interchangeable, so their outgoing speeds are one unknown and not two.

∣vB′∣=∣vC′∣=u(2) |\vect v_B'| = |\vect v_C'| = u \tag{2}

Each of BB and CC leaves along its own line of centres, at the angle θ\theta to the axis, so each carries ucos⁡θu\cos\theta of momentum along the axis and its full speed uu into the energy, while the two transverse components cancel against each other. With every mass equal to mm, momentum along the axis reads

mv=mv′+2mucos⁡θ  ⟹  v=v′+2ucos⁡θ,(3) mv = mv'+2mu\cos\theta \;\Longrightarrow\; v = v'+2u\cos\theta, \tag{3}

and the collision being elastic, kinetic energy reads

12mv2=12mv′2+2⋅12mu2  ⟹  v2=v′2+2u2.(4) \frac12 mv^2 = \frac12 mv'^2+2\cdot\frac12 mu^2 \;\Longrightarrow\; v^2 = v'^2+2u^2. \tag{4}
Step 3Solving the pair for uu

Substituting v′=v−2ucos⁡θv'=v-2u\cos\theta from (3) into (4) and collecting terms in uu leaves a quadratic whose nonzero root is the common recoil speed uu of (2).

v2=(v−2ucos⁡θ)2+2u20=−4uvcos⁡θ+u2(4cos⁡2θ+2)0=u[−4vcos⁡θ+u(4cos⁡2θ+2)]\begin{align*}v^2 &= (v-2u\cos\theta)^2+2u^2 \\ 0 &= -4uv\cos\theta+u^2\bigl(4\cos^2\theta+2\bigr) \\ 0 &= u\Bigl[-4v\cos\theta+u\bigl(4\cos^2\theta+2\bigr)\Bigr]\end{align*}

Discarding the trivial root u=0u=0 (no collision at all) leaves

u=4vcos⁡θ4cos⁡2θ+2=2vcos⁡θ2cos⁡2θ+1.(5) u = \frac{4v\cos\theta}{4\cos^2\theta+2} = \frac{2v\cos\theta}{2\cos^2\theta+1}. \tag{5}
Step 4Disc AA’s velocity in terms of θ\theta, then η\eta

Substituting (5) back into (3) and simplifying over the common denominator gives v′v' in terms of cos⁡2θ\cos^2\theta alone; (1) then converts it to η\eta.

v′=v−2ucos⁡θ=v−4vcos⁡2θ2cos⁡2θ+1=v(1−2cos⁡2θ)2cos⁡2θ+1\begin{align*}v' &= v-2u\cos\theta = v-\frac{4v\cos^2\theta}{2\cos^2\theta+1} \\ &= \frac{v(1-2\cos^2\theta)}{2\cos^2\theta+1}\end{align*}
1−2cos⁡2θ=1−2(1−η24)=η2−222cos⁡2θ+1=2(1−η24)+1=6−η22\begin{align*}1-2\cos^2\theta &= 1-2\Bigl(1-\frac{\eta^2}{4}\Bigr) = \frac{\eta^2-2}{2} \\ 2\cos^2\theta+1 &= 2\Bigl(1-\frac{\eta^2}{4}\Bigr)+1 = \frac{6-\eta^2}{2}\end{align*}
v′=−v(2−η2)6−η2v' = -\dfrac{v(2-\eta^2)}{6-\eta^2}
(6)
Step 5The sign of v′v' across the allowed range of η\eta

On 1≤η≤21\le\eta\le2 the denominator 6−η26-\eta^2 stays positive throughout, so the sign of v′v' follows the sign of −(2−η2)=η2−2-(2-\eta^2)=\eta^2-2 alone. Disc AA recoils (moves backward, v′<0v'<0) for η<2\eta<\sqrt2, stops exactly (v′=0v'=0) at η=2\eta=\sqrt2, and continues forward (v′>0v'>0) for η>2\eta>\sqrt2.

Check

At the grazing limit η→2\eta\to2, θ→90∘\theta\to90^\circ and cos⁡θ→0\cos\theta\to0: the lines of centers become perpendicular to v\vect v, so a contact impulse along either one can carry no component along v\vect v at all, and the boxed formula gives v′→−v(2−4)/(6−4)=vv'\to-v(2-4)/(6-4)=v, disc AA passing through untouched, consistent with a contact that (in this limit) exerts no force along the direction of approach.

Remark

The whole problem collapses to two scalar unknowns, v′v' and the common recoil speed uu, only because the mirror symmetry between BB and CC removes the sideways component of AA’s motion before any equation is written down; a BB and CC placed asymmetrically about the line of v\vect v would need a transverse momentum equation as well, and disc AA would leave along a genuinely different line than the one it arrived on.