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Drag Costs More Going Up

Irodov 1.104DifficultyDifficulty 4 of 5UniquenessUniqueness 4 of 5

Problem Irodov 1.104

A body of mass mm is thrown vertically upward with initial speed v0v_0. Air drag on the body has magnitude kv2kv^2 at any instant its speed is vv, for some constant kk, and always opposes the body’s velocity. Find the speed v′v' with which the body returns to its starting height.

The throw: the body leaves the starting level (dashed) straight upward with the given speed v_0, and the question is the speed it has when it comes back down through that same level.

The throw: the body leaves the starting level (dashed) straight upward with the given speed v0v_0, and the question is the speed it has when it comes back down through that same level.

Given
  • mm
  • v0v_0
  • drag =kv2=kv^2, always opposing v\vect v
Find
The return speed v′v' at the starting height

Solution

Step 1Equation of motion on the way up
Rising: gravity m g and the drag kv^2 both point downward, since drag opposes the upward velocity v (drawn with a small angular offset from m g purely so the two are visible as separate arrows).

Rising: gravity mgm\vect g and the drag kv2kv^2 both point downward, since drag opposes the upward velocity v\vect v (drawn with a small angular offset from mgm\vect g purely so the two are visible as separate arrows).

Take yy positive upward from the launch point. While rising, both gravity and drag point downward (figure above), so with v=dy/dt>0v=dy/dt>0,

mdvdt=−mg−kv2.m\frac{dv}{dt} = -mg-kv^2.

Using dv/dt=v dv/dydv/dt=v\,dv/dy and separating variables,

v dvg+(k/m)v2=−dy.\frac{v\,dv}{g+(k/m)v^2} = -dy.
Step 2The height reached

Integrate from the launch point y=0y=0, v=v0v=v_0, to the top y=Hy=H, v=0v=0:

∫v00v dvg+(k/m)v2=−∫0Hdy.\int_{v_0}^{0}\frac{v\,dv}{g+(k/m)v^2} = -\int_0^H dy.

The left side is a logarithm of the denominator, evaluated at its two limits:

m2k[ln⁡ ⁣(g+kmv2)]v00=−H⟹m2kln⁡gg+(k/m)v02=−H.\frac{m}{2k}\left[\ln\!\left(g+\frac{k}{m}v^2\right)\right]_{v_0}^{0} = -H \quad\Longrightarrow\quad \frac{m}{2k}\ln\frac{g}{g+(k/m)v_0^2} = -H.
H=m2kln⁡ ⁣(1+kv02mg)H = \dfrac{m}{2k}\ln\!\left(1+\dfrac{kv_0^2}{mg}\right)
(1)
Step 3Equation of motion on the way down
Falling: gravity m g still points downward, while the drag kv^2, opposing the now downward velocity v, points up. Velocity and drag are drawn slightly off vertical so they read as arrows separate from m g.

Falling: gravity mgm\vect g still points downward, while the drag kv2kv^2, opposing the now downward velocity v\vect v, points up. Velocity and drag are drawn slightly off vertical so they read as arrows separate from mgm\vect g.

Take y′y' positive downward from the top, so y′=0y'=0 is the top and y′=Hy'=H is the launch height. While falling, gravity points down (in the +y′+y' sense) and drag opposes the downward velocity, so it points up (figure above):

mdvdt=mg−kv2.m\frac{dv}{dt} = mg-kv^2.

Rewriting the acceleration as v dv/dy′v\,dv/dy' again and separating the variables,

v dvg−(k/m)v2=dy′.\frac{v\,dv}{g-(k/m)v^2} = dy'.
Step 4The return speed

Integrate from the top y′=0y'=0, v=0v=0, to the launch height y′=Hy'=H, v=v′v=v':

∫0v′v dvg−(k/m)v2=∫0Hdy′⟹−m2kln⁡g−(k/m)v′2g=H.\int_0^{v'}\frac{v\,dv}{g-(k/m)v^2} = \int_0^{H} dy' \quad\Longrightarrow\quad -\frac{m}{2k}\ln\frac{g-(k/m)v'^2}{g} = H.

Substituting (1) for HH and canceling the common factor m/(2k)m/(2k),

−ln⁡g−(k/m)v′2g=ln⁡ ⁣(1+kv02mg)⟹gg−(k/m)v′2=1+kv02mg.-\ln\frac{g-(k/m)v'^2}{g} = \ln\!\left(1+\frac{kv_0^2}{mg}\right) \quad\Longrightarrow\quad \frac{g}{g-(k/m)v'^2} = 1+\frac{kv_0^2}{mg}.

Cross multiplying and solving for v′2v'^2,

g=(g−kmv′2)(1+kv02mg)g⋅mgmg+kv02=g−kmv′2kmv′2=g−mg2mg+kv02=gkv02mg+kv02\begin{align*}g &= \left(g-\frac{k}{m}v'^2\right)\left(1+\frac{kv_0^2}{mg}\right) \\ g\cdot\frac{mg}{mg+kv_0^2} &= g-\frac{k}{m}v'^2 \\ \frac{k}{m}v'^2 &= g-\frac{mg^2}{mg+kv_0^2} = \frac{gkv_0^2}{mg+kv_0^2}\end{align*}
v′2=gv02mg+kv02⋅m=v021+kv02/(mg)v'^2 = \frac{gv_0^2}{mg+kv_0^2}\cdot m = \frac{v_0^2}{1+kv_0^2/(mg)}
v′=v01+kv02/(mg)v' = \dfrac{v_0}{\sqrt{1+kv_0^2/(mg)}}
(2)
Check

As k→0k\to0 (no drag), v′→v0v'\to v_0, recovering ordinary free flight where the body returns at launch speed. Also v′<v0v'<v_0 for any k>0k>0, as it must: drag removes mechanical energy on both the way up and the way down, so the body cannot return faster than it left.

Remark

The ratio v′2/v02=1/(1+kv02/mg)v'^2/v_0^2=1/(1+kv_0^2/mg) depends on kk, v0v_0, mm and gg only through the single dimensionless combination kv02/(mg)kv_0^2/(mg), even though the intermediate height HH needed its own logarithm to reach. That collapse happens because integrating v dvv\,dv against either g+(k/m)v2g+(k/m)v^2 (Step 2) or g−(k/m)v2g-(k/m)v^2 (Step 4) produces a logarithm with the exact same prefactor m/(2k)m/(2k) out front; setting the two results equal through the common height HH cancels that shared prefactor, leaving only the logarithms’ arguments to combine.