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Two Accelerations Trade Places Mid Flight

Irodov 1.30DifficultyDifficulty 3 of 5UniquenessUniqueness 4 of 5

Problem Irodov 1.30

For the same projectile as before, launched at speed v0v_0 and angle α\alpha above the horizontal under constant gravity gg with no air drag, sketch how three quantities vary over the flight, from launch (t=0t=0) to landing (t=τt=\tau): the modulus of the normal acceleration wnw_n, the modulus of the tangential acceleration wτw_\tau, and the signed projection wvw_v of the total acceleration onto the velocity direction.

Given
  • v0v_0
  • α\alpha
  • gg (as in the foregoing problem)
Find
the shapes of wn(t)w_n(t), wτ(t)w_\tau(t), wv(t)w_v(t) over 0≤t≤τ0\le t\le\tau

Solution

Step 1Velocity components through the flight

Only gravity acts, so the horizontal component of velocity is constant while the vertical component decreases linearly; both come from one integration of g\vect g.

vx=v0cos⁡α,vy(t)=v0sin⁡α−gt,v(t)=vx2+vy(t)2(1)v_x = v_0\cos\alpha, \qquad v_y(t) = v_0\sin\alpha-gt, \qquad v(t)=\sqrt{v_x^2+v_y(t)^2} \tag{1}
Step 2The signed projection of g\vect g on the velocity

Projecting the constant acceleration g=−gj\vect g=-g\vect j onto the unit vector v/v\vect v/v isolates this component directly.

wv=g⋅vv=−g vy(t)v(t)\begin{align*}w_v &= \vect g\cdot\frac{\vect v}{v} = \frac{-g\,v_y(t)}{v(t)}\end{align*}
wv(t)=g(gt−v0sin⁡α)v02cos⁡2α+(v0sin⁡α−gt)2w_v(t) = \dfrac{g\bigl(gt-v_0\sin\alpha\bigr)}{\sqrt{v_0^2\cos^2\alpha+(v_0\sin\alpha-gt)^2}}
(2)
Step 3Tangential and normal moduli from the same projection

The tangential modulus is the same component read as a magnitude, so (2) already carries it:

wτ(t)=∣wv(t)∣w_\tau(t) = |w_v(t)|

The normal modulus is the component of g\vect g perpendicular to v\vect v. Taking the cross product of the two vectors and dividing by vv isolates that component, and with g=−gj\vect g = -g\vect j only the horizontal piece of v\vect v survives the product.

wn=∣g×v∣v=∣(−gj)×(vxi+vyj)∣v(t)=g vxv(t)\begin{align*}w_n &= \frac{\bigl|\vect g\times\vect v\bigr|}{v} = \frac{\bigl|(-g\vect j)\times(v_x\vect i+v_y\vect j)\bigr|}{v(t)}\\ &= \frac{g\,v_x}{v(t)}\end{align*}

Substituting vx=v0cos⁡αv_x=v_0\cos\alpha and v(t)v(t) from (1) gives the normal modulus in terms of the givens.

wn(t)=g v0cos⁡αv02cos⁡2α+(v0sin⁡α−gt)2w_n(t) = \dfrac{g\,v_0\cos\alpha}{\sqrt{v_0^2\cos^2\alpha+(v_0\sin\alpha-gt)^2}}
(3)

Squaring and adding (2) and (3) shows the pair accounts for the whole of g\vect g, since vx2+vy2=v2v_x^2+v_y^2=v^2:

wn2+wv2=g2vx2v2+g2vy2v2=g2(4)w_n^2+w_v^2 = \frac{g^2 v_x^2}{v^2}+\frac{g^2 v_y^2}{v^2} = g^2 \tag{4}
Step 4Values at the launch, the peak and the landing
The three curves over one flight, sketched for α=30°: w_n (gold), w_τ (royal) and w_v (sky). w_τ is dashed from the peak onward, where w_v crosses zero and the two run together.

The three curves over one flight, sketched for α=30∘\alpha=30^\circ: wnw_n (gold), wτw_\tau (royal) and wvw_v (sky). wτw_\tau is dashed from the peak onward, where wvw_v crosses zero and the two run together.

At t=0t=0 and t=τt=\tau, v(t)=v0v(t)=v_0 by the symmetry of (1); at the peak t=τ/2t=\tau/2, vy=0v_y=0 so v(t)=v0cos⁡αv(t)=v_0\cos\alpha. Putting those three speeds into (3) and (2), and taking wτ=∣wv∣w_\tau=|w_v|,

wn(0)=wn(τ)=gcos⁡α,wn(τ/2)=gwτ(0)=wτ(τ)=gsin⁡α,wτ(τ/2)=0wv(0)=−gsin⁡α,wv(τ/2)=0,wv(τ)=gsin⁡α\begin{align*}w_n(0)=w_n(\tau) &= g\cos\alpha, \qquad w_n(\tau/2) = g \\ w_\tau(0)=w_\tau(\tau) &= g\sin\alpha, \qquad w_\tau(\tau/2) = 0 \\ w_v(0) &= -g\sin\alpha,\qquad w_v(\tau/2)=0, \qquad w_v(\tau) = g\sin\alpha\end{align*}

Over the flight, wnw_n rises smoothly from gcos⁡αg\cos\alpha to gg at the peak and back to gcos⁡αg\cos\alpha at landing; wτw_\tau falls from gsin⁡αg\sin\alpha to 00 at the peak and climbs back, a V touching the axis; and wvw_v runs from −gsin⁡α-g\sin\alpha through 00 at the peak up to +gsin⁡α+g\sin\alpha, crossing zero exactly where wτw_\tau bottoms out, all sketched in the figure.

Three curves sketched in the figure above
Check

At every instant wn2+wv2=g2w_n^2+w_v^2=g^2 by (4), so the total acceleration always has magnitude gg, as it must for free fall; at the peak this gives wn=gw_n=g, wv=0w_v=0 exactly, matching Step 4.

Remark

wτw_\tau and wvw_v carry the same information, ∣wv∣|w_v| against wvw_v, but the modulus throws away the one fact worth keeping: whether the body is still speeding up or already slowing down. A speedometer reads the speed vv itself, never wτw_\tau directly; it is the sign of wvw_v, not wτw_\tau, that tells you which side of the peak the body is on.