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NACA 23012 Airfoil Design Analysis by Himanshu Modi is a document available to read on EtoBox.
What is NACA 23012 Airfoil Design Analysis about?
The document describes a term project to analyze the aerodynamic characteristics of a NACA 23012 airfoil using vortex panel methods. It will: 1. Generate a NACA 23012 airfoil model with 19 panels on the upper and lower surfaces and calculate boundary layer parameters. 2. Use a vortex panel method and simple turbulence model to predict the airfoil
- Author
- Himanshu Modi
- Language
- EN