06 October 2025 11:26:50 AM

naca_test():
  C++ version
  Test naca().

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_test():
  Normal end of execution.

06 October 2025 11:26:50 AM