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Reading Launch Speed Off a Parabola's Shape

Irodov 1.27DifficultyDifficulty 3 of 5UniquenessUniqueness 3 of 5

Problem Irodov 1.27

A particle moves in the xyxy plane under a constant acceleration w\vect w of magnitude ww, directed along the negative yy axis. Its trajectory is the parabola y=ax−bx2y=ax-bx^2, with aa and bb known positive constants. Find the particle’s velocity (magnitude) at the instant it passes through the origin.

The parabolic path through the origin. The launch velocity v_0 at O is tangent to the path there; the constant acceleration w points along - j throughout the flight.

The parabolic path through the origin. The launch velocity v0\vect v_0 at OO is tangent to the path there; the constant acceleration w\vect w points along −j-\vect j throughout the flight.

Given
  • y=ax−bx2y=ax-bx^2
  • w∥−j\vect w\parallel-\vect j, ∣w∣=w|\vect w|=w
Find
v0v_0 at the origin

Solution

Step 1Write the motion in components

With w=−wj\vect w=-w\vect j constant and no acceleration along xx, the two coordinates evolve independently from the launch instant t=0t=0 at the origin, where the velocity components are v0xv_{0x} and v0yv_{0y}.

x(t)=v0xt,y(t)=v0yt−w2t2x(t) = v_{0x}t, \qquad y(t) = v_{0y}t-\frac{w}{2}t^2
Step 2Eliminate tt and match the given trajectory

Solving the xx equation for tt and substituting into y(t)y(t) expresses the path as a function of xx alone, which must be identical to the stated parabola for every xx.

t=xv0xy=v0yxv0x−w2(xv0x)2=v0yv0x x−w2v0x2 x2\begin{align*}t &= \frac{x}{v_{0x}} \\ y &= v_{0y}\frac{x}{v_{0x}}-\frac{w}{2}\left(\frac{x}{v_{0x}}\right)^2 \\ &= \frac{v_{0y}}{v_{0x}}\,x-\frac{w}{2v_{0x}^2}\,x^2\end{align*}

Matching coefficients with y=ax−bx2y=ax-bx^2 term by term gives two equations for the launch components, and they are the crux of the problem: the parabola’s two constants are exactly the two things the launch velocity has to supply.

a=v0yv0x,b=w2v0x2a=\dfrac{v_{0y}}{v_{0x}},\qquad b=\dfrac{w}{2v_{0x}^2}
(1)
Step 3Solve for the launch components

The second of (1) isolates v0xv_{0x} directly, and the first of them then gives v0yv_{0y} in terms of it.

v0x2=w2bv0x=w2bv0y=a v0x=aw2b\begin{align*} v_{0x}^2 &= \frac{w}{2b} \\ v_{0x} &= \sqrt{\frac{w}{2b}} \\ v_{0y} &= a\,v_{0x} \\ &= a\sqrt{\frac{w}{2b}} \tag{2}\end{align*}
Step 4Combine into the launch speed

The speed at the origin is the root sum of squares of the two components (2).

v02=v0x2+v0y2=w2b+a2w2b=(1+a2)w2b\begin{align*}v_0^2 &= v_{0x}^2+v_{0y}^2 \\ &= \frac{w}{2b}+a^2\frac{w}{2b} \\ &= \frac{(1+a^2)w}{2b}\end{align*}
v0=(1+a2)w2bv_0 = \sqrt{\dfrac{(1+a^2)w}{2b}}
(3)
Check

Dimensionally aa is a plain slope and bb has units of inverse length, so w/bw/b carries units of length2^2/time2^2, and w/2b\sqrt{w/2b} is a speed, as required. As a→0a\to0 the launch is purely horizontal (v0y=0v_{0y}=0) and v0→w/2b=v0xv_0\to\sqrt{w/2b}=v_{0x}, consistent with Step 3.

Remark

The parabola’s own shape already fixes the launch velocity completely: bb alone sets the horizontal speed through v0x=w/2bv_{0x}=\sqrt{w/2b} (how sharply the path curves, for a given ww), and a=tan⁡θ0a=\tan\theta_0 is just the launch angle’s slope. This is the same reading used to time a gravity-driven projectile from its trajectory’s coefficients alone, without ever separately measuring a speed or an angle.