[F1 Master]

Hello mates,
I can't load the airfoil data at ANSYS with 3D Curve. It pops me up an error message.
What happen? I tried to fix my dimensions but nothing.
Below i will attach you the txt file:
NACA 0012 WITH ANGLE OF ATTACK.txt

Thanks...

[Светлана]

Your first coordinate is x=10. It looks funny (attached). Changing that coordinate to x=1.0 helped me to make it work, this is what works for me:

#Group Point X_cord Y-cord Z-cord
1 1 1.000 0.0000 0.0000
1 2 0.9961 0.0006 0.0000
1 3 0.9843 0.0023 0.0000
1 4 0.9649 0.0050 0.0000
1 5 0.9382 0.0086 0.0000
1 6 0.9045 0.0131 0.0000
1 7 0.8645 0.0181 0.0000
1 8 0.8187 0.0236 0.0000
1 9 0.7679 0.0293 0.0000
1 10 0.7129 0.0350 0.0000
1 11 0.6545 0.0407 0.0000
1 12 0.5937 0.0460 0.0000
1 13 0.5314 0.0508 0.0000
1 14 0.4686 0.0547 0.0000
1 15 0.4063 0.0578 0.0000
1 16 0.3455 0.0596 0.0000
1 17 0.2871 0.0600 0.0000
1 18 0.2321 0.0589 0.0000
1 19 0.1813 0.0562 0.0000
1 20 0.1355 0.0519 0.0000
1 21 0.0955 0.0460 0.0000
1 22 0.0618 0.0389 0.0000
1 23 0.0351 0.0305 0.0000
1 24 0.0157 0.0211 0.0000
1 25 0.0039 0.0109 0.0000
1 26 0.0000 0.0000 0.0000
1 27 0.0039 -0.0109 0.0000
1 28 0.0157 -0.0211 0.0000
1 29 0.0351 -0.0305 0.0000
1 30 0.0618 -0.0389 0.0000
1 31 0.0955 -0.0460 0.0000
1 32 0.1355 -0.0519 0.0000
1 33 0.1813 -0.0562 0.0000
1 34 0.2321 -0.0589 0.0000
1 35 0.2871 -0.0600 0.0000
1 36 0.3455 -0.0596 0.0000
1 37 0.4063 -0.0578 0.0000
1 38 0.4686 -0.0547 0.0000
1 39 0.5314 -0.0508 0.0000
1 40 0.5937 -0.0460 0.0000
1 41 0.6545 -0.0407 0.0000
1 42 0.7129 -0.0350 0.0000
1 43 0.7679 -0.0293 0.0000
1 44 0.8187 -0.0236 0.0000
1 45 0.8645 -0.0181 0.0000
1 46 0.9045 -0.0131 0.0000
1 47 0.9382 -0.0086 0.0000
1 48 0.9649 -0.0050 0.0000
1 49 0.9843 -0.0023 0.0000
1 50 0.9961 -0.0006 0.0000
1 0

[alaspina]

Make sure that you use this format:

#Group Point X_cord Y-cord Z-cord
All ones
(good option for meshing is to split top surface from bottom surface)

[Светлана]

To make it easier to use I attached the coordinates as a file below.