MATLAB: NACA-0012 Airfoil PRessure ANalysis
MATLAB: NACA-0012 Airfoil PRessure ANalysis
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This project is designed around compressibility approximation using Pradntl-Glauert, Karman Tsien, and Laitones Rules. These are some of the main approximations for compressibility correction that are used within the study of compressible aerodynamics. Utilizing different MACH values different curves are generated to determine the most accurate rule.
SOLVes And Plots for M=n
SOLVes And Plots for M=n
Solves Critical Pressure Values
Solves Critical Pressure Values
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