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Angular Momentum Grows as Time Squared

Irodov 1.186DifficultyDifficulty 3 of 5UniquenessUniqueness 3 of 5

Problem Irodov 1.186

A ball of mass mm is launched from a point OO with initial speed v0v_0 at angle α\alpha above the horizontal, moving freely under constant gravitational acceleration gg with air drag neglected. Find the magnitude of the ball’s angular momentum about OO as a function of the elapsed time tt. Then evaluate this angular momentum at the instant the ball reaches the highest point of its trajectory, for m=130 gm=130\text{ g}, α=45∘\alpha=45^\circ, v0=25 m/sv_0=25\text{ m/s}.

The parabolic flight path from the launch point O, showing the position r and velocity v at the general point P reached at time t. At P_max, the highest point, v is horizontal.

The parabolic flight path from the launch point OO, showing the position r\vect r and velocity v\vect v at the general point PP reached at time tt. At PmaxP_{\mathrm{max}}, the highest point, v\vect v is horizontal.

Given
  • mm
  • α\alpha
  • v0\vect v_0
  • gg
Find
M(t)M(t); MM at the highest point for m=130 gm=130\text{ g}, α=45∘\alpha=45^\circ, v0=25 m/sv_0=25\text{ m/s}

Solution

Step 1Position and velocity from launch

Take OO as the origin with xx horizontal and yy vertically upward, and let i\vect i, j\vect j, k\vect k be the unit vectors along xx, yy and the outward normal to the plane of flight. The standard projectile equations under constant gg give the four components.

x(t)=v0cos⁡α t,y(t)=v0sin⁡α t−12gt2,vx(t)=v0cos⁡α,vy(t)=v0sin⁡α−gt.(1)\begin{aligned} x(t) &= v_0\cos\alpha\, t, & y(t) &= v_0\sin\alpha\, t - \frac{1}{2}gt^2, \\ v_x(t) &= v_0\cos\alpha, & v_y(t) &= v_0\sin\alpha - gt. \end{aligned} \tag{1}

The two vectors the angular momentum is built from are those components on the two in-plane unit vectors, with no k\vect k part at any time, since the flight never leaves the plane.

r(t)=x(t) i+y(t) jv(t)=vx(t) i+vy(t) j(2)\begin{aligned} \vect r(t) &= x(t)\,\vect i + y(t)\,\vect j \\ \vect v(t) &= v_x(t)\,\vect i + v_y(t)\,\vect j \end{aligned} \tag{2}
Step 2The angular momentum as a cross product

The angular momentum about OO is M=m r×v\vect M = m\,\vect r\times\vect v. Expanding that cross product from (2) gives four terms, one for each pairing of the two unit vectors.

r×v=(x i+y j)×(vx i+vy j)=xvx(i×i)+xvy(i×j)+yvx(j×i)+yvy(j×j)=(xvy−yvx) k\begin{align*} \vect r\times\vect v &= (x\,\vect i + y\,\vect j)\times(v_x\,\vect i + v_y\,\vect j) \\ &= xv_x(\vect i\times\vect i) + xv_y(\vect i\times\vect j) + yv_x(\vect j\times\vect i) + yv_y(\vect j\times\vect j) \\ &= (xv_y - yv_x)\,\vect k \tag{3}\end{align*}

Substituting the components of (1) into (3) and multiplying out both products,

xvy=v0cos⁡α t (v0sin⁡α−gt)=v02sin⁡αcos⁡α t−gv0cos⁡α t2,yvx=(v0sin⁡α t−12gt2)v0cos⁡α=v02sin⁡αcos⁡α t−12gv0cos⁡α t2.\begin{align*}xv_y &= v_0\cos\alpha\,t\,(v_0\sin\alpha-gt) = v_0^2\sin\alpha\cos\alpha\,t - gv_0\cos\alpha\,t^2, \\ yv_x &= \left(v_0\sin\alpha\,t-\frac{1}{2}gt^2\right)v_0\cos\alpha = v_0^2\sin\alpha\cos\alpha\,t - \frac{1}{2}gv_0\cos\alpha\,t^2.\end{align*}

Subtracting cancels the identical first terms, and (3) turns the difference into the one surviving component of M\vect M.

xvy−yvx=−gv0cos⁡α t2+12gv0cos⁡α t2=−12gv0cos⁡α t2Mz(t)=m(xvy−yvx)=−12mgv0cos⁡α t2(4)\begin{aligned} xv_y - yv_x &= -gv_0\cos\alpha\,t^2 + \frac{1}{2}gv_0\cos\alpha\,t^2 = -\frac{1}{2}gv_0\cos\alpha\,t^2 \\ M_z(t) = m(xv_y-yv_x) &= -\frac{1}{2}mgv_0\cos\alpha\,t^2 \end{aligned} \tag{4}

Only the magnitude of the angular momentum is asked for, so

M(t)=∣Mz(t)∣=12mgv0t2cos⁡αM(t) = |M_z(t)| = \dfrac{1}{2}mgv_0t^2\cos\alpha
(5)
Step 3The time of flight to the highest point

The highest point is reached when the vertical velocity vanishes, vy=0v_y=0 in (1), giving

ttop=v0sin⁡αg.t_{\mathrm{top}} = \frac{v_0\sin\alpha}{g}.
Step 4The angular momentum at the highest point

Substituting ttopt_{\mathrm{top}} into (5) gives MM at the apex.

Mtop=12mgv0cos⁡α(v0sin⁡αg)2=mv03sin⁡2αcos⁡α2g\begin{align*}M_{\mathrm{top}} = \frac{1}{2}mgv_0\cos\alpha\left(\frac{v_0\sin\alpha}{g}\right)^2 &= \frac{mv_0^3\sin^2\alpha\cos\alpha}{2g}\end{align*}

With m=0.130 kgm=0.130\text{ kg}, α=45∘\alpha=45^\circ (sin⁡2α=1/2\sin^2\alpha=1/2, cos⁡α=2/2\cos\alpha=\sqrt2/2), v0=25 m/sv_0=25\text{ m/s} and g=9.8 m/s2g=9.8\text{ m/s}^2 substituted in,

Mtop=(0.130)(25)3(1/2)(2/2)2(9.8) kg⋅m2/sM_{\mathrm{top}} = \frac{(0.130)(25)^3(1/2)(\sqrt2/2)}{2(9.8)}\ \text{kg}\cdot\text{m}^2/\text{s}
Mtop=mv03sin⁡2αcos⁡α2g=37 kg⋅m2/sM_{\mathrm{top}} = \dfrac{mv_0^3\sin^2\alpha\cos\alpha}{2g} = 37\text{ kg}\cdot\text{m}^2/\text{s}
(6)
Check

Differentiating the signed result (4) gives dMz/dt=−mgv0cos⁡α tdM_z/dt=-mgv_0\cos\alpha\,t. Independently, gravity is the only force present, and a force −mgj^-mg\hat{\vect j} acting at horizontal offset x(t)x(t) exerts torque N=−mgx(t)=−mgv0cos⁡α tN=-mgx(t)=-mgv_0\cos\alpha\,t about OO: the two expressions for dMz/dtdM_z/dt agree, confirming Step 2 without repeating its cross-product algebra. Also M(0)=0M(0)=0, as it must be, since r=0\vect r=\vect 0 at the launch point itself.

Remark

The torque of gravity about OO grows only linearly with time, N=−mgv0cos⁡α tN=-mgv_0\cos\alpha\,t, yet the angular momentum it builds grows quadratically, M∝t2M\propto t^2, because MM is the running time-integral of that torque. The same pattern appears in x(t)x(t) of (1), which is linear in tt while y(t)y(t) (built from the same constant gg) carries a t2t^2 term: one more power of tt appears every time a constant rate is integrated once more.