EVERYTHING CONNECTED – Numorpho's Book of Business

Airfoil GPT-5 generated

Interactive Airfoil with Cd Estimation

Can you draw a two dimensional airfoil (Aerofoil) with parameters that can be changed to modify its coefficient of drag (Cd)

Camber (m): 0.02

Camber Position (p): 0.4

Thickness (t): 0.12

Chord Length (m): 1.0

Angle of Attack (°): 5

August 10, 2025

numorpho

Steve Wegryn says:

August 10, 2025 at 7:45 pm

Nitin, this is really cool!! I think angle of attack is
Represented incorrectly. Leading edge increasingly up is positive, not negative. Let me know if you disagree.

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