Terminal Velocity
v = √(2mg/(ρ C_d A)) at steady drag = weight.
Inputs
Results
m/s
44.551
How to Use This Calculator
- Enter the object mass (kg).
- Set the drag coefficient Cd -- sphere ~0.47, skydiver flat ~1.0, skydiver streamlined ~0.7.
- Enter the cross-sectional area (m2) and air density (kg/m3) -- 1.225 at sea level.
- Review terminal velocity in m/s and mph.
- Reduce area or Cd to increase terminal velocity -- relevant for vehicle aerodynamics and projectile ballistics.
How the result changes with C_d
| C_d | m/s |
|---|---|
| 0.51 | 65.493 |
| 1.76 | 35.221 |
| 3.25 | 25.919 |
| 4.5 | 22.027 |
What each input means
- Mass (kg)
- Mass of the falling object in kilograms. Average adult is about 75 kg.
- C_d
- Drag coefficient. A skydiver spread-eagle is about 1.0-1.3; head-down dive is about 0.4.
- Area (m²)
- Frontal area.
- ρ air (kg/m³)
- Sea level ~1.225.
How this is calculated
Formula
v_t = √(2mg / (ρ × C_d × A))Related Calculators
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