idrag input file
asample2 - an elliptic load distribution
1                 input mode
1                 write flag
1                 symmetry flag
1                 load flag
0.                x cg position
0.25              center of pressure for airfoil sections
0.15              reference area
0.15              reference chord
1                 number of panels
0   0   0         x,y,z for 4 corners of panel 1
0   0.5 0
0.2 0.5 0
0.2 0   0
10                number of vortices for panel 1
0                 vortex spacing for panel 1
11                number of loads for panel 1
0.0000    1.0000  load station  1, load  1, for panel 1
0.1000    0.9950  load station  2, load  2, for panel 1
0.2000    0.9798  load station  3, load  3, for panel 1
0.3000    0.9539  load station  4, load  4, for panel 1
0.4000    0.9165  load station  5, load  5, for panel 1
0.5000    0.8660  load station  6, load  6, for panel 1
0.6000    0.8000  load station  7, load  7, for panel 1
0.7000    0.7141  load station  8, load  8, for panel 1
0.8000    0.6000  load station  9, load  9, for panel 1
0.9000    0.4359  load station 10, load 10, for panel 1
1.0000    0.0000  load station 11, load 11, for panel 1
