CristianMoncio
Guest
Good morning, they're cristian, mechanical engineering student at the bari polytechnic. I'm finding problems in entering data through text document in ansys, since every time I try to insert it gives me as an error "error reading coordinates file" . the nodes I copied them from airfoil tools, since I need to build a wing profile, so I don't understand why I don't read them.
I cover below the list of nodes I have found:
1,000,000,000,000,000,000,000,000
0.999756
0.999023
0.997802 0.000469
0.996095 0.000832
0.993903
0.991228
0.988072
0.984438
0.980330 0.004145
0.975752
0.970707 0.00129
0.965201 0.007252
0.959238
0.952825 0.009744
0.945966 0.011105
0.938669
0.930941 0.014039
0.922788 0.015605
0.914218 0.017230
0.905240
0.895862 0.020641
0.886092 0.022419
0.875941 0.024239
0.865417 0.026096
0.854532
0.843294 0.029903
0.831716 0.031844
0.819807 0.033804
0.807581 0.035777
0.795047
0.782219 0.039747
0.769109 0.041734
0.755730 0.043716
0.742094 0.045689
0.728216 0.047648
0.71407 0.049588
0.699783 0.051505
0.685258 0.053394
0.670545 0.055251
0.655659
0.6414 0.058850
0.625426 0.060584
0.610110 0.062268
0.594680 0.063897
0.579153 0.065468
0.563542 0.066977
0.547865 0.068418
0.532136 0.069789
0.516372 0.071085
0.500587 0.072303
0.484799
0.469022 0.074486
0.453273 0.075446
0.437567 0.076312
0.421921 0.077082
0.406350 0.077752
0.390796 0.078315
0.375297 0.078743
0.359920 0.079032
0.344680 0.079180
0.329594 0.079186
0.314678 0.079051
0.299948 0.078773
0.285418
0.27106
0.257025
0.243191 0.076259
0.229618
0.216321 0.074181
0.203313
0.190609 0.071582
0.178222 0.070096
0.166164 0.068490
0.154449 0.066770
0.143089 0.064940
0.132094 0.063005
0.121477 0.060970
0.111248 0.058842
0.101418
0.091996 0.054325
0.082992 0.051950
0.074415 0.049504
0.066273 0.046994
0.058573 0.044427
0.051324
0.044532
0.038203 0.036441
0.032343 0.033704
0.026958
0.022051 0.02815
0.017628 0.025348
0.013692
0.0245 0.019707
0.007292
0.004833 0.014049
0.002870 0.011224
0.00104
0.000439
-0.000030 0.002790
0.000000
0.000523 -0.002741
0.001535 -0.005395
0.003033 -0.007961
0.005015 -0.010439
0.007479 -0.0128
0.010421 -0.015126
0.013838 -0.017334
0.017725 -0.019451
0.022078 -0.021476
0.026892 -0.023408
0.032161 -0.025246
0.037880 -0.026990
0.044042 -0.028639
0.050641 -0.030193
0.057669 -0.031651
0.065120 -0.033014
0.072985 -0.034280
0.081257 -0.035451
0.089927 -0.036527
0.098987 -0.037507
0.108427 -0.038392
0.118239 -0.039185
0.128412 -0.039884
0.138937 -0.040493
0.149805 -0.041012
0.161004 -0.041444
0.172524 -0.041791
0.184354 -0.042054
0.196484 -0.042238
0.208902 -0.042343
0.221596 -0.042375
0.234555 -0.042335
0.247768 -0.042228
0.261221 -0.042058
0.274904 -0.041827
0.288802 -0.041541
0.302904 -0.041203
0.317197 -0.040817
0.331668 -0.040389
0.346303 -0.039923
0.361089 -0.039422
0.376013 -0.038892
0.391061 -0.038336
0.406269 -0.037757
0.421645 -0.037134
0.437099 -0.036467
0.452619 -0.035757
0.468187 -0.035009
0.483790 -0.034227
0.499413 -0.033414
0.515039 -0.032573
0.530654 -0.031708
0.546243 -0.030821
0.561791 -0.029917
0.577282 -0.028997
0.592701 -0.028066
0.608033 -0.027125
0.623264 -0.026176
0.638377 -0.025224
0.653358 -0.024269
0.668193 -0.023313
0.682867 -0.022360
0.697364 -0.021410
0.711672 -0.020466
0.725775 -0.019529
0.739659 -0.018600
0.753311 -0.017681
0.766718 -0.016774
0.779864 -0.015880
0.792738 -0.014999
0.805327 -0.014133
0.817617 -0.013284
0.829596 -0.012451
0.841253 -0.011637
0.852575 -0.010842
0.863551 -0.010068
0.874170 -0.009314
0.884421 -0.008583
0.894293 -0.007875
0.903777 -0.007191
0.912862 -0.006532
0.921540 -0.005900
0.929801 -0.005294
0.937637 -0.004717
0.945040 -0.004169
0.952002 -0.003650
0.958516 -0.003163
0.964576 -0.002708
0.970174 -0.002285
0.975305 -0.001896
0.979964 -0.001541
0.984145 -0.001222
0.987845 -0.000938
0.991060 -0.000691
0.993785 -0.000481
0.996020 -0.000308
0.997760 -0.000174
0.999004 -0.000077
0.999751 -0.000019
1,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000
the tool I use on the workbench is "fluid flow (fluent)" and from there I open new design modeler, as I saw in a guide on youtube. despite following all the steps, he does not have this problem (here is the link of the video I followed until the minute 13
).
I need your help, because I am novice with this software and unfortunately the professor of my internship that should follow me, not only explained this software in a very old version, so what I am using is completely different, but in addition it is irreperible always.
Thank you in advance.
I cover below the list of nodes I have found:
1,000,000,000,000,000,000,000,000
0.999756
0.999023
0.997802 0.000469
0.996095 0.000832
0.993903
0.991228
0.988072
0.984438
0.980330 0.004145
0.975752
0.970707 0.00129
0.965201 0.007252
0.959238
0.952825 0.009744
0.945966 0.011105
0.938669
0.930941 0.014039
0.922788 0.015605
0.914218 0.017230
0.905240
0.895862 0.020641
0.886092 0.022419
0.875941 0.024239
0.865417 0.026096
0.854532
0.843294 0.029903
0.831716 0.031844
0.819807 0.033804
0.807581 0.035777
0.795047
0.782219 0.039747
0.769109 0.041734
0.755730 0.043716
0.742094 0.045689
0.728216 0.047648
0.71407 0.049588
0.699783 0.051505
0.685258 0.053394
0.670545 0.055251
0.655659
0.6414 0.058850
0.625426 0.060584
0.610110 0.062268
0.594680 0.063897
0.579153 0.065468
0.563542 0.066977
0.547865 0.068418
0.532136 0.069789
0.516372 0.071085
0.500587 0.072303
0.484799
0.469022 0.074486
0.453273 0.075446
0.437567 0.076312
0.421921 0.077082
0.406350 0.077752
0.390796 0.078315
0.375297 0.078743
0.359920 0.079032
0.344680 0.079180
0.329594 0.079186
0.314678 0.079051
0.299948 0.078773
0.285418
0.27106
0.257025
0.243191 0.076259
0.229618
0.216321 0.074181
0.203313
0.190609 0.071582
0.178222 0.070096
0.166164 0.068490
0.154449 0.066770
0.143089 0.064940
0.132094 0.063005
0.121477 0.060970
0.111248 0.058842
0.101418
0.091996 0.054325
0.082992 0.051950
0.074415 0.049504
0.066273 0.046994
0.058573 0.044427
0.051324
0.044532
0.038203 0.036441
0.032343 0.033704
0.026958
0.022051 0.02815
0.017628 0.025348
0.013692
0.0245 0.019707
0.007292
0.004833 0.014049
0.002870 0.011224
0.00104
0.000439
-0.000030 0.002790
0.000000
0.000523 -0.002741
0.001535 -0.005395
0.003033 -0.007961
0.005015 -0.010439
0.007479 -0.0128
0.010421 -0.015126
0.013838 -0.017334
0.017725 -0.019451
0.022078 -0.021476
0.026892 -0.023408
0.032161 -0.025246
0.037880 -0.026990
0.044042 -0.028639
0.050641 -0.030193
0.057669 -0.031651
0.065120 -0.033014
0.072985 -0.034280
0.081257 -0.035451
0.089927 -0.036527
0.098987 -0.037507
0.108427 -0.038392
0.118239 -0.039185
0.128412 -0.039884
0.138937 -0.040493
0.149805 -0.041012
0.161004 -0.041444
0.172524 -0.041791
0.184354 -0.042054
0.196484 -0.042238
0.208902 -0.042343
0.221596 -0.042375
0.234555 -0.042335
0.247768 -0.042228
0.261221 -0.042058
0.274904 -0.041827
0.288802 -0.041541
0.302904 -0.041203
0.317197 -0.040817
0.331668 -0.040389
0.346303 -0.039923
0.361089 -0.039422
0.376013 -0.038892
0.391061 -0.038336
0.406269 -0.037757
0.421645 -0.037134
0.437099 -0.036467
0.452619 -0.035757
0.468187 -0.035009
0.483790 -0.034227
0.499413 -0.033414
0.515039 -0.032573
0.530654 -0.031708
0.546243 -0.030821
0.561791 -0.029917
0.577282 -0.028997
0.592701 -0.028066
0.608033 -0.027125
0.623264 -0.026176
0.638377 -0.025224
0.653358 -0.024269
0.668193 -0.023313
0.682867 -0.022360
0.697364 -0.021410
0.711672 -0.020466
0.725775 -0.019529
0.739659 -0.018600
0.753311 -0.017681
0.766718 -0.016774
0.779864 -0.015880
0.792738 -0.014999
0.805327 -0.014133
0.817617 -0.013284
0.829596 -0.012451
0.841253 -0.011637
0.852575 -0.010842
0.863551 -0.010068
0.874170 -0.009314
0.884421 -0.008583
0.894293 -0.007875
0.903777 -0.007191
0.912862 -0.006532
0.921540 -0.005900
0.929801 -0.005294
0.937637 -0.004717
0.945040 -0.004169
0.952002 -0.003650
0.958516 -0.003163
0.964576 -0.002708
0.970174 -0.002285
0.975305 -0.001896
0.979964 -0.001541
0.984145 -0.001222
0.987845 -0.000938
0.991060 -0.000691
0.993785 -0.000481
0.996020 -0.000308
0.997760 -0.000174
0.999004 -0.000077
0.999751 -0.000019
1,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000,000
the tool I use on the workbench is "fluid flow (fluent)" and from there I open new design modeler, as I saw in a guide on youtube. despite following all the steps, he does not have this problem (here is the link of the video I followed until the minute 13
I need your help, because I am novice with this software and unfortunately the professor of my internship that should follow me, not only explained this software in a very old version, so what I am using is completely different, but in addition it is irreperible always.
Thank you in advance.