Drag Equation Calculator

Calculate drag force on objects moving through fluids using the drag equation

Drag Force Parameters

Select fluid or use custom density

Density of the fluid medium

Velocity of object relative to fluid

Select object shape for drag coefficient

Dimensionless drag coefficient

Cross-sectional area perpendicular to flow

Drag Force Results

Drag Force

0.000
Newtons (N)
0.000
pounds-force (lbf)

Additional Parameters

Reynolds Number:0
Terminal Velocity:0.00 m/s
Dynamic Pressure:0.00 Pa

Formula used: Fd = ½ × ρ × v² × A × Cd

Input values: ρ=1.225kg/m³, v=0.00m/s, A=0.0000m², Cd=0.47

Flow Analysis

Example Calculation

Skydiver with Parachute

Fluid: Air (ρ = 1.225 kg/m³)

Velocity: 20 m/s

Parachute area: 7 m²

Drag coefficient: 1.3 (parachute)

Calculation

Fd = ½ × ρ × v² × A × Cd

Fd = ½ × 1.225 × 20² × 7 × 1.3

Fd = ½ × 1.225 × 400 × 7 × 1.3

Fd = 2,191.5 N

Drag Coefficient Values

Streamlined

Cd = 0.04

Highly aerodynamic shapes

Sphere

Cd = 0.47

Smooth sphere

Cylinder

Cd = 0.82

Long cylinder, cross flow

Cube

Cd = 1.05

Bluff body

Applications

1

Aerospace

Aircraft and spacecraft design

2

Automotive

Vehicle aerodynamics and fuel efficiency

3

Sports

Equipment design and performance

4

Civil Engineering

Building and bridge wind loads

Calculation Tips

Use cross-sectional area perpendicular to flow direction

Drag coefficient depends on Reynolds number and shape

Consider surface roughness for accurate Cd values

Account for compressibility at high velocities

Understanding the Drag Equation

What is Drag Force?

Drag force is the resistance force that opposes the motion of an object through a fluid (liquid or gas). It acts parallel to and in the opposite direction of the object's velocity relative to the fluid.

Key Factors

  • Fluid density (ρ) - denser fluids create more drag
  • Velocity² (v²) - drag increases with square of velocity
  • Reference area (A) - larger cross-section increases drag
  • Drag coefficient (Cd) - depends on object shape

Drag Equation

Fd = ½ × ρ × v² × A × Cd

  • Fd: Drag force (N)
  • ρ: Fluid density (kg/m³)
  • v: Relative velocity (m/s)
  • A: Reference area (m²)
  • Cd: Drag coefficient (dimensionless)

Note: The ½ factor comes from the dynamic pressure term in fluid mechanics

Types of Drag

Form Drag

Due to pressure difference around object

Dominant for bluff bodies like spheres, cubes

Skin Friction

Due to viscous effects at surface

Important for streamlined bodies

Induced Drag

Due to lift generation in 3D flow

Significant for wings and airfoils