Calculate fall time, impact velocity, and distance with aerodynamic quadratic drag, terminal velocity (v_term = √(2mg/ρCdA)), and air resistance with the free Free Fall with Air Resistance Calculator.
120.0 mph • 193.1 km/h • Impact Speed: 53.4 m/s (99.6% of v_term)
119.5 mph
Actual flight duration
+7.5s air drag penalty
313.3 mph in vacuum
99.4% of object weight
Mechanical energy
In atmospheric physics and fluid mechanics, free fall with air resistance describes the downward trajectory of an object subjected to both gravitational attraction (\(F_g = m g\)) and opposing aerodynamic fluid drag (\(F_d\)). In high-speed subsonic regimes, aerodynamic resistance scales with the square of velocity (quadratic drag):
As the falling body accelerates, drag force grows until it exactly equals gravitational weight (\(F_d = m g\)). At this equilibrium, net acceleration drops to zero (\(a = 0\)), and the body coasts downward at a constant speed known as Terminal Velocity (\(v_{\text{term}}\)).
| Kinematic Metric | Formula | Description |
|---|---|---|
| Terminal Velocity (\(v_{\text{term}}\)) | $$v_{\text{term}} = \sqrt{\frac{2 m g}{\rho C_d A}}$$ | Maximum asymptotic speed in \(\text{m/s}\) |
| Velocity vs. Time \(v(t)\) | $$v(t) = v_{\text{term}} \tanh\left(\frac{g t}{v_{\text{term}}}\right)$$ | Instantaneous speed after \(t\) seconds |
| Distance Fallen \(y(t)\) | $$y(t) = \frac{v_{\text{term}}^2}{g} \ln\left(\cosh\left(\frac{g t}{v_{\text{term}}}\right)\right)$$ | Total vertical distance fallen after \(t\) |
| Velocity vs. Distance \(v(y)\) | $$v(y) = v_{\text{term}} \sqrt{1 - e^{-2 g y / v_{\text{term}}^2}}$$ | Impact speed from drop height \(y\) |
| Fall Time from Height \(h\) | $$t(h) = \frac{v_{\text{term}}}{g} \operatorname{arcosh}\left(e^{g h / v_{\text{term}}^2}\right)$$ | Elapsed flight time to reach ground |
How skydivers control terminal velocity by adjusting body geometry:
Maximizes surface drag, giving a stable terminal velocity of \(\approx 54\text{ m/s}\) (\(120\text{ mph} \approx 194\text{ km/h}\)). Reaches \(95\%\) of terminal velocity in \(\approx 8\text{ seconds}\) over a \(300\text{-meter}\) drop.
Minimizes cross-sectional area, surging terminal velocity up to \(\approx 90\text{ m/s}\) (\(200\text{ mph} \approx 324\text{ km/h}\)).
Determines the exact cross-sectional area (\(A\)) required to slow payload descents to safe touchdown speeds (\(v_{\text{term}} \le 5\text{ m/s}\)).
Replaces inaccurate vacuum approximations (\(v = \sqrt{2gh}\)) with true drag-limited impact velocities and kinetic energies.
Models emergency drone parachute recovery descent profiles and spent rocket booster atmospheric re-entry deceleration curves.
Computes instantaneous speeds via \(v(t) = v_{\text{term}}\tanh(gt/v_{\text{term}})\) with zero numerical rounding errors.
Displays side-by-side time and velocity differences between atmospheric fall and ideal vacuum free fall.
Adjusts fluid density (\(\rho\)) and gravity (\(g\)) across Earth sea level, high altitude, Moon, Mars, and Jupiter.
Why stratospheric skydivers break the sound barrier before slowing down:
When Felix Baumgartner stepped out of his capsule at \(38,969\text{ meters}\) (\(127,852\text{ ft}\)), atmospheric density was less than \(1.5\%\) of sea level (\(\rho \approx 0.018\text{ kg/m}^3\)). With negligible air resistance, his terminal velocity soared to over \(1,350\text{ km/h}\), allowing him to reach a peak velocity of \(1,357.6\text{ km/h}\) (\(\text{Mach } 1.25\)), breaking the speed of sound in free fall. As he descended into the denser troposphere, increasing air density progressively lowered his terminal velocity to \(\approx 200\text{ km/h}\) long before parachute deployment.
Comprehensive answers to common questions about free fall with air resistance, terminal velocity formulas, quadratic aerodynamic drag, and vacuum comparisons.