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Library / Fluid Mechanics / FLU-11

Fluid Mechanics

Drag force

Resistance of a fluid to a moving body.

Ref
FLU-11
Rev
v1
Field
Fluid Mechanics
Result
FD [N]

ρ is the fluid density, v the speed relative to the fluid, C_D the drag coefficient and A the reference area that the coefficient was defined with (usually the frontal area for a vehicle). F_D acts opposite to the motion. The force is ½ρv² multiplied by C_D A, so it is dynamic pressure times an effective area.

Resistance of a fluid to a moving body. It grows with the square of speed, so the power needed grows with the cube.

Calculator

Solve for
N
kg/m³
0.012,000
m/s
0.11,000
0.012
m²
0.0011,000
  • Power to overcome the drag, F_D v45.94 kW
  • Drag at twice the speed3,675 N

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Drag force (N) current value 918.8 N
ρFluid densityKey driver
7.51,500,000
AReference area
0.459459,000
vSpeed
0.00368368,000
CDDrag coefficient
30.66,130
  • At 50 m/s (180 km/h) this body feels 919 N, and overcoming it takes 46 kW. At 100 m/s the force is 3.7 kN and the power 368 kW, eight times more.
  • Because power rises as v³, a small increase in top speed costs a lot of engine: 26 % more speed needs about double the power.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (N)Local stepChange in result
ρ Fluid density0.01 to 2,000 kg/m³7.51,500,0001,500,000+10%+10 %
A Reference area0.001 to 1,000 m²0.4594459,400459,400+10%+10 %
v Speed0.1 to 1,000 m/s0.003675367,500367,500+10%+21 %
CD Drag coefficient0.01 to 2 30.636,1256,094+10%+10 %

Sweep of Speed

Speed (m/s)Drag force (N)
0.10.003675
0.31620.03675
10.3675
3.1623.675
1036.75
31.62367.5
1003,675
316.236,750
1,000367,500

Sweep one variable

Drag force (N)Hover, touch, or use the arrow keys on the chart
0100k200k300k 0.11101001000 Speed (m/s), log scale now 918.8

Variables and how each one contributes

FD

Drag force

Result · N

What the equation gives you. Everything else feeds it.

ρ

Fluid density

kg/m³ · typical 0.01 to 2,000

The density of the fluid, in kg/m³. Directly proportional: the same shape in water feels about 800 times the drag it feels in air at the same speed.

v

Speed

m/s · typical 0.1 to 1,000

The speed relative to the fluid. Squared: doubling the speed quadruples the force, and the power needed to overcome it is cubed. A 10 % rise in v raises F by 21 %.

CD

Drag coefficient

· typical 0.01 to 2

The drag coefficient, a number set by the shape and Reynolds number. Directly proportional: halving the drag coefficient halves the force at any speed.

A

Reference area

m² · typical 0.001 to 1,000

The reference area on which C_D is based, in m². Directly proportional: a larger frontal area gives proportionally more drag.

Worked example with the values above

  1. Dynamic pressure: ½ρv² = ½ × 1.225 × 50² = 1,531 Pa.
  2. Effective area: C_D A = 0.3 × 2 = 0.6 m².
  3. FD = 1,531 × 0.6 = 918.8 N.

Assumptions and limits

  • Steady flow at a constant C_D, which changes with Reynolds number and, near the speed of sound, with Mach number.
  • The reference area is the same one used to define the quoted C_D.

Common mistakes

  • Using C_D with the wrong reference area (frontal area for a car, wing area for an aircraft).
  • Forgetting that power depends on the cube of the speed.

Statistics and uncertainty

F ∝ ρ v² C_D A, so the speed dominates: a 1 % error in v gives 2 % in F, against 1 % for each of the others. C_D itself is rarely known to better than 5 to 10 %, and varies with Reynolds number, yaw angle and surface condition.

Where it is used

  • Estimating vehicle drag and the engine power needed to overcome it.
  • Predicting the speed at which a falling body reaches terminal velocity.

Maths you need

  • Dynamic pressure: ½ρv²
  • Dimensionless coefficients: a number set by shape

Related formulas

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