Reply To: Error: “Cannot open airfoil table naca16016.dat” in Fluent Tutorial 33.2 (VBM)

[asp89]

I think so here is dat file I have, it looks the same as the required format 
naca16016
2
cl
10000
0.01
19
-180    -0.726282
-8    -0.726282
-7    -0.622431
-6    -0.518581
-5    -0.41473
-4    -0.31088
-3    -0.207029
-2    -0.103178
-1    -0.000672425 
0    0.104523
1    0.208374
2    0.312224
3    0.405996
4    0.499767
5    0.590514
6    0.681261
7    0.749592
8    0.817924
180    0.817924
cd
10000
0.01
19
-180    0.052773
-8    0.052773
-7    0.0448664
-6    0.0399598
-5    0.0266581
-4    0.0180578
-3    0.00917065
-2    0.00714089
-1    0.00541159
0    0.00525418
1    0.00541159
2    0.00714089
3    0.00917065
4    0.0180578
5    0.0266581
6    0.0369598
7    0.0448664
8    0.052773
180    0.052773