Drag force calculator

Pick a shape with a typical drag coefficient or enter your own, then give the frontal area, the speed and the fluid density (air at sea level by default). The calculator gives the drag force in newtons and pound-force, the power it takes at that speed and the terminal velocity a body of the given mass would reach when falling.

m²
Speed unit
kg/m³
kg
Drag force385.88 N
In pound-force
86.75 lbf
Power to overcome drag
11,576.3 W
Terminal velocity
42.78 m/s
Terminal velocity in km/h
154 km/h
Terminal velocity in mph
95.7 mph
Drag coefficient used
1
Weight
784.53 N

Runs in your browser: nothing you enter is sent anywhere.

How to use it

  1. Choose a shape, or “Own drag coefficient” and type Cd.
  2. Enter the frontal area — the area of the shadow the object casts in the direction of motion.
  3. Enter the speed and pick m/s, km/h or mph.
  4. Keep 1.225 kg/m³ for air at sea level, or enter another density (fresh water is about 1000 kg/m³).
  5. Enter the mass if you want the terminal velocity.

Formulas

  • Drag force F = ½ × ρ × v² × Cd × A
  • Power P = F × v
  • Terminal velocity v_t = √(2 × m × g ÷ (ρ × Cd × A)), with g = 9.80665 m/s²
Shape Cd
Streamlined body 0.04
Half-sphere, round side forward 0.42
Sphere 0.47
Cone, point forward 0.50
Cube, edge forward 0.80
Long cylinder, side-on 0.82
Cube, face forward 1.05
Short cylinder, end-on 1.15
Flat plate, face-on 1.28

Worked example

A skydiver-like body: Cd = 1.0, A = 0.7 m², v = 30 m/s in air of 1.225 kg/m³.

  • F = 0.5 × 1.225 × 30² × 1.0 × 0.7 = 385.88 N (86.75 lbf)
  • P = 385.88 × 30 = 11,576.3 W
  • With 80 kg (weight 784.53 N): v_t = √(2 × 80 × 9.80665 ÷ (1.225 × 1.0 × 0.7)) = 42.78 m/s, 154 km/h

Tips

  • Area and Cd go together. Car makers often quote the product Cd·A; if you have it, enter Cd = 1 and that number as the area.
  • Density changes with altitude and temperature. In the standard atmosphere air at 2000 m has about 1.007 kg/m³, 18 % less than at sea level, so drag is 18 % lower.
  • Terminal velocity ignores buoyancy, which is fine in air but not for slow objects sinking in water.

Frequently asked questions

What is the drag equation?

F = ½ × ρ × v² × Cd × A, where ρ is the fluid density, v the speed, Cd the drag coefficient and A the frontal area. Air at sea level and 15 °C has ρ = 1.225 kg/m³.

How is terminal velocity calculated?

A falling body stops accelerating when drag equals its weight, so v_t = √(2·m·g ÷ (ρ·Cd·A)). For 80 kg, Cd 1.0 and 0.7 m² in sea-level air it is 42.78 m/s, about 154 km/h.

Why does doubling the speed quadruple the drag?

Drag grows with v², and the power needed to overcome it grows with v³. Going from 30 to 60 m/s multiplies the force by 4 and the power by 8.

Where do the drag coefficients come from?

They are typical measured values for simple shapes at high Reynolds numbers. Real objects vary with surface roughness and speed, so treat them as estimates and enter your own Cd when you have a better figure.

More in Math

All tools in this category: Math ·Updated November 4, 2026

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