22 May 2014 12:08:14 PM NACA_PRB: C++ version Test the NACA library. TEST01 NACA4_SYMMETRIC evaluates y(x) for a NACA symmetric airfoil defined by a 4-digit code. Data saved in file 'symmetric_data.txt' Created command file 'symmetric_commands.txt' TEST02 NACA4_CAMBERED evaluates (xu,yu) and (xl,yl) for a NACA cambered airfoil defined by a 4-digit code. Data saved in file 'cambered_data.txt' Created command file 'cambered_commands.txt' NACA_PRB: Normal end of execution. 22 May 2014 12:08:14 PM