! This demo program reads the naca6403_Re20k.csv and writes it to ! an output file naca6403_Re20k.C81. Both files are in the Samples/ directory. program demo2 use libC81 implicit none integer, parameter :: rows = 19 integer, parameter :: cols = 4 integer, parameter :: nMach = cols-1 integer :: i,j type(C81_class) :: C81 real, dimension(rows,cols) :: A ! Read airfoil data from CSV file A=getTable('Samples/NACA6409.csv',rows,cols) ! Allocate arrays allocate(C81%MaL(nMach)) allocate(C81%MaD(nMach)) allocate(C81%MaM(nMach)) allocate(C81%AL(rows-1)) allocate(C81%AD(rows-1)) allocate(C81%AM(rows-1)) allocate(C81%CL(rows-1,nMach)) allocate(C81%CD(rows-1,nMach)) allocate(C81%CM(rows-1,nMach)) ! Specify airfoil name C81%airfoilName = 'NACA6409' ! Copy values from read array to variables C81%MaL = A(1,2:) C81%MaD = C81%MaL C81%MaM = C81%MaL C81%AL = A(2:,1) C81%AD = C81%AL C81%AM = C81%AL do j=2,cols do i=2,rows C81%CL(i-1,j-1) = A(i,j) enddo enddo C81%CD = C81%CL C81%CM = C81%CL ! Write airfoil data to C81 file call c81%writefile('Samples/NACA6409.C81') end program demo2