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Lecture 35, Navier Stokes Airfoil Simulation 


Basically, this is a study to see if the 1933 wind tunnel
measurements of airfoils for coefficient of lift CL and
coefficient of drag CD can be reproduced by computer
simulation.


Airfoil 0015

Testing formulas for 0015 airfoil
rotate_prime.java



Create data file for airfoil at a specific angle and grid:
w0015grid.java

Build a PDE analysis grid around the airfoil:
w0015vert.java



w0015grid_java.out
w0015a22.grid
w0015vert_java.out




w0015b22_grid_java.out
w0015b22.grid
w0015b22_vert_java.out




w0015c22_grid_java.out
w0015c22.grid
w0015c22_vert_java.out





w0015b00.grid
w0015b00_vert_java.out

References:
NACA-460 1933 78 airfoils 
NACA-824 1945 Airfoil Summary


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