Drag Force Calculator

Enter drag coefficient, air density, reference area, and velocity to compute aerodynamic drag force in newtons.

Inputs

Standard sea-level air = 1.225 kg/m³. Water = 998 kg/m³.

Results

Fill in the inputs and press Calculate.

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Summary

Enter drag coefficient, air density, reference area, and velocity to compute aerodynamic drag force in newtons.

How it works

  1. Select a preset shape (sphere, cylinder, flat plate, streamlined body) or enter a custom drag coefficient.
  2. Enter the air (or fluid) density in kg/m³ — 1.225 kg/m³ is standard sea-level air.
  3. Enter the reference (frontal) area in square metres.
  4. Enter the object velocity in metres per second.
  5. Read the drag force in newtons and the dynamic pressure in the results panel.

Use cases

  • Estimate aerodynamic drag on a vehicle at highway speed.
  • Size parachutes for load drops or recovery systems.
  • Compute drag on a sports ball (baseball, soccer ball, golf ball).
  • Check drag on a cyclist or runner for performance analysis.
  • Validate CFD results against hand calculations.
  • Teach the drag equation in physics or engineering courses.

Frequently Asked Questions

Last updated: 2026-06-10 · Reviewed by Nham Vu