AbraCalc

Terminal Velocity Calculator

Calculate terminal velocity using the drag equation: v_t = √(2mg / ρC_dA). Enter mass, gravity, drag coefficient, fluid density and cross-section area.

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APA

AbraCalc. (2026). Terminal Velocity Calculator [Online calculator]. Retrieved from https://abracalc.com/calculator/terminal-velocity-calculator/

BibTeX

@misc{abracalc-terminal-velocity-calculator, author = {AbraCalc}, title = {Terminal Velocity Calculator}, year = {2026}, howpublished = {\url{https://abracalc.com/calculator/terminal-velocity-calculator/}} }

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How to use this tool

  1. Enter mass, gravitational acceleration, drag coefficient cd, fluid density ρ and cross-sectional area a in the fields above.
  2. Results update instantly as you type — or click Calculate.
  3. Read your terminal velocity and the full breakdown beneath it.

An object reaches terminal velocity when drag force equals gravity. The formula is v_t = √(2mg / ρC_dA), where m is mass, g gravity, ρ fluid density, C_d the drag coefficient, and A the cross-sectional area.

Formula

vt = √(2mg ÷ ρ Cd A)

Where: m = mass (kg), g = gravitational acceleration (m/s²), ρ = fluid density (kg/m³), Cd = drag coefficient, A = cross-sectional area (m²).

How it works

Terminal velocity is reached when the upward drag force on a falling object exactly equals its downward weight. Setting the drag equation Fdrag = ½ρCdAv2 equal to gravitational force mg and solving for v gives the formula above.

The calculator converts the result to km/h (multiply by 3.6) and mph (multiply by 2.23694). It assumes a rigid body in steady laminar or turbulent flow; in practice, shape changes, spin, or altitude variation can alter the true terminal speed.

Worked example

  1. Given: mass m = 80 kg, g = 9.81 m/s², drag coefficient Cₙ = 1.0, fluid density ρ = 1.225 kg/m³, cross-section A = 0.7 m².
  2. Compute numerator: 2 × 80 × 9.81 = 1569.6.
  3. Compute denominator: 1.225 × 1.0 × 0.7 = 0.8575.
  4. vₜ = √(1569.6 ÷ 0.8575) = √(1830.38...) ≈ 42.79 m/s.

Terminal velocity = 42.79 m/s.

Common mistakes to avoid

  • Using a drag coefficient for a sphere (C_d approx 0.47) for a non-spherical object like a skydiver or a falling leaf, which can be off by a factor of 2 or more.
  • Entering body mass in grams instead of kilograms, or cross-sectional area in cm2 instead of m2, producing a result that is orders of magnitude wrong.
  • Assuming terminal velocity is reached instantly; it is an asymptotic limit that an object approaches exponentially, so a falling object is still accelerating (slowly) even at 90% of terminal velocity.

Key terms

Terminal velocity
The constant maximum speed reached by a falling object when drag force equals gravitational force.
Drag coefficient (Cₙ)
A dimensionless number representing how aerodynamically streamlined a body is. A sphere is ~0.47; a skydiver in freefall position is ~1.0.
Fluid density (ρ)
Mass per unit volume of the medium the object moves through. Air at sea level is approximately 1.225 kg/m³.
Cross-sectional area (A)
The projected area of the object perpendicular to the direction of motion, which determines how much fluid the object must push aside.
Drag force
The resistive force exerted by a fluid on a moving body, proportional to the square of velocity at high Reynolds numbers.

Frequently asked questions

What is a typical skydiver terminal velocity?
In a spread-eagle position (Cd≈1.0, A≈0.7 m²) around 55–60 m/s (200 km/h). Head-down (Cd≈0.7, A≈0.3 m²) can reach ~80 m/s (290 km/h).
What drag coefficient should I use?
Sphere: 0.47, cube: 1.05, flat disk: 1.17, skydiver prone: ~1.0, streamlined body: 0.04–0.1.

References & sources