CFD Aerodynamics Analysis Tool

Simulating Lift & Drag on 2D Airfoils

Input Parameters

Airfoil Profile (NACA 4-Digit)

Angle of Attack (α): 5°

Airspeed (v) m/s

Air Density (ρ) kg/m³

Chord Length (c) m

Lift (L)

N

Drag (D)

N

L/D Ratio

Cʟ

Cᴅ

Theory & Step-by-Step Solution

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