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What is NACA 4424 Airfoil Data Analysis about?

This document contains airfoil coordinate data for the NACA 4424 airfoil profile, listing the x and y coordinates along the airfoil surface from the leading edge at x=0 to the trailing edge at x=1. The profile is symmetric about the x-axis with maximum thickness of 0.15606 located at x=0.4.

Author

karthickraja

Language

EN