26 February 2024 0 3K Report

Hi, I am a masters student. I need some guidance for my thesis work. I want to work on the leading-edge morphing of a cambered airfoil (NACA 4412). I have done a 2D analysis of the NACA 4412 airfoil using CFD, but I am not able to perform morphing on it. Basically, i need help with leading edge morphed geometry of NACA 4412 so i can do 2D analysis on the cambered airfoil (NACA 4412) morphed from the leading edge

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