Parachute aerodynaimc calculator

Parachute Size Calculator

Parachute Size Calculator

About Wing Loading

Wing loading is the ratio of the jumper’s weight to the area of the parachute, typically measured in pounds per square foot (lbs/sq.ft). It’s a critical factor in determining how a parachute will perform.

Low wing loading (below 1.0) provides slower, more forgiving descents, ideal for beginners.

Moderate wing loading (1.0-1.3) offers a balance of performance and safety, suitable for most recreational jumpers.

High wing loading (above 1.3) results in faster descents and more responsive handling, but requires greater skill to control safely.

Reference Chart: Recommended Wing Loading

Experience Level Conservative Moderate Aggressive
Student/Novice 0.7 – 0.8 0.8 – 0.9 0.9 – 1.0
Intermediate 0.9 – 1.0 1.0 – 1.1 1.1 – 1.2
Experienced 1.0 – 1.2 1.2 – 1.4 1.4 – 1.6
Expert 1.2 – 1.5 1.5 – 1.8 1.8 – 2.2+
Parachute Descent Calculator

Interactive Parachute Descent Calculator

Input Parameters

Calculation Results

Terminal Velocity:
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Descent Time:
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Drag Force:
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Area-to-Weight Ratio:
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Deceleration at Opening:
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(Assuming free-fall at 50 m/s before deployment)
Safety Assessment:
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Parachute Aerodynamics Calculator

Parachute Aerodynamics Calculator

Calculator
Theory

Input Parameters

Typical values: Round (1.75), Flat (0.8), Cruciform (1.1), Parafoil (1.4)
Combined mass of jumper, equipment, and parachute

Results

Parachute Area:
Air Density: kg/m³
Terminal Velocity: m/s ( km/h)
Drag Force: N
Descent Time: seconds
Wing Loading: kg/m²

Parachute Aerodynamics Theory

Key Principles

Parachute aerodynamics involve the balance of gravitational force and aerodynamic drag. When these forces reach equilibrium, the parachute descends at a constant speed called terminal velocity.

Important Equations

Terminal Velocity: The speed at which the drag force equals the gravitational force.

Vt = √(2mg / (ρ·Cd·A))

Where:

  • m = mass (kg)
  • g = gravitational acceleration (9.81 m/s²)
  • ρ = air density (kg/m³)
  • Cd = drag coefficient (dimensionless)
  • A = parachute area (m²)

Drag Force:

Fd = 0.5 · ρ · v² · Cd · A

Air Density Calculation:

Air density decreases with altitude according to the barometric formula. At sea level, air density is approximately 1.225 kg/m³.

Parachute Types and Drag Coefficients

Different parachute designs have varying drag coefficients:

  • Round (hemispherical): Cd ≈ 1.75
  • Flat circular: Cd ≈ 0.8
  • Cruciform: Cd ≈ 1.1
  • Parafoil (ram-air): Cd ≈ 1.4

Wing Loading

Wing loading is the total suspended weight divided by the surface area. It’s an important factor in determining the performance of a parachute. Lower wing loading generally results in slower descent rates but can affect maneuverability.