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error reading coordinate file

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Old   March 31, 2017, 02:44
Default error reading coordinate file
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Hi

when i am importing a coordinate file using 3D curve option a window is popping out saying that error reading coordinate file.
Can u plzz give a solution for this problem.
I had attached the file also
Attached Files
File Type: txt copy11.txt (1.7 KB, 178 views)
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Old   April 1, 2017, 15:34
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Quote:
Originally Posted by pradeepsama View Post
Hi

when i am importing a coordinate file using 3D curve option a window is popping out saying that error reading coordinate file.
Can u plzz give a solution for this problem.
I had attached the file also
What code is this for?
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Old   April 1, 2017, 15:42
Default error
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these are airfoil coordinates.
can anybody help plzz
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Old   April 1, 2017, 15:48
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You need to post more information such as what code you are using to get help. You haven't provide any information.
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Old   April 1, 2017, 15:58
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i am opening the work bench and using modal analysis
and i am importing the coordinate file by first making proper arrangement of columns in ms excel and after importing the file when i am joining the points by "lines through point" option i am able to join some point after that i am getting an error called points are self intersecting.
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Old   April 2, 2017, 19:09
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remove the last line of code and try once more, it mite solve
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Old   August 14, 2017, 15:36
Default DS error reading coordinates file
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Awanerv
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Hi all

I have the same error of this topic DS error reading coordinates file.

I dont understand the file NACA-4412 is works fine to import but my other file is get this error.

I search in the CFD forum but nothing can solve my problem here some solution:

The txt file must be saved as ANSI not UNICODE(it saves like that by default)

  • Put comment # at the beginning of each column( such as #x, #y etc)
  • The last row must be 1 0 that means erase the column relative to x,y,z coordinates because they are the same of the first one( I am assuming that you have created an airfoil with closed trailing edge)
  • Save the file as ANSI not unicode.


I dont know where my error in the file Clark Y.txt


I generate from the site aerofoil tools


my ansys version is 17.1, excel version 2013.


I salve the file in txt tab delimited and nothing works.


thanks
Attached Files
File Type: txt NACA-4412.txt (615 Bytes, 214 views)
File Type: txt Clark Y.txt (3.0 KB, 95 views)
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Old   November 24, 2018, 16:18
Post Naca 4415
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Quote:
Originally Posted by awanerv View Post
Hi all

I have the same error of this topic DS error reading coordinates file.

I dont understand the file NACA-4412 is works fine to import but my other file is get this error.

I search in the CFD forum but nothing can solve my problem here some solution:

The txt file must be saved as ANSI not UNICODE(it saves like that by default)

  • Put comment # at the beginning of each column( such as #x, #y etc)
  • The last row must be 1 0 that means erase the column relative to x,y,z coordinates because they are the same of the first one( I am assuming that you have created an airfoil with closed trailing edge)
  • Save the file as ANSI not unicode.


I dont know where my error in the file Clark Y.txt


I generate from the site aerofoil tools


my ansys version is 17.1, excel version 2013.


I salve the file in txt tab delimited and nothing works.


thanks
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Old   November 24, 2018, 16:19
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Quote:
Originally Posted by ismailzor View Post


Hi dude. I have a problem this naca 4415 text file's. Can you help me for create this file. Please .................................................. ....................................... Thanks a lot...............................
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Old   September 11, 2019, 04:57
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Hi Pradeep,

I had a similar error. The fix was to use same format of numbers as used in ansys; that is if a comma or dot is the correct input for decimal place.
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Old   October 1, 2019, 10:35
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Quote:
Originally Posted by Adithya_B View Post
Hi Pradeep,

I had a similar error. The fix was to use same format of numbers as used in ansys; that is if a comma or dot is the correct input for decimal place.
That's the answer.
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Old   May 14, 2020, 01:21
Default easy solution
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Quote:
Originally Posted by pradeepsama View Post
Hi

when i am importing a coordinate file using 3D curve option a window is popping out saying that error reading coordinate file.
Can u plzz give a solution for this problem.
I had attached the file also
when u download coordinates from airfoil plotter
you will have repeated coordinates in the excel file , you just need to remove that one repeated co ordinate point , thats simple
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Old   January 8, 2021, 07:50
Default Help with coordinate file!
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Hey guys!
So im trying to upload this coordinate file in DM, but when I do I get the error that id is found in coordinates file. I have tried both commas and points but it didn't work. can anyone help me? I dont know how to add the file so ill do it like this:
#e387coords
#group #point #x_cord #y_cord #z_cord
1 1 1,00000 0,00000 0
1 2 0,99677 0,00043 0
1 3 0,98729 0,00180 0
1 4 0,97198 0,00423 0
1 5 0,95128 0,00763 0
1 6 0,92554 0,01184 0
1 7 0,89510 0,01679 0
1 8 0,86035 0,02242 0
1 9 0,82183 0,02866 0
1 10 0,78007 0,03540 0
1 11 0,73567 0,04249 0
1 12 0,68922 0,04975 0
1 13 0,64136 0,05696 0
1 14 0,59272 0,06390 0
1 15 0,54394 0,07020 0
1 16 0,49549 0,07546 0
1 17 0,44767 0,07936 0
1 18 0,40077 0,08173 0
1 19 0,35505 0,08247 0
1 20 0,31078 0,08156 0
1 21 0,26813 0,07908 0
1 22 0,22742 0,07529 0
1 23 0,18906 0,07037 0
1 24 0,15345 0,06448 0
1 25 0,12094 0,05775 0
1 26 0,09185 0,05033 0
1 27 0,06643 0,04238 0
1 28 0,04493 0,03408 0
1 29 0,02748 0,02562 0
1 30 0,01423 0,01726 0
1 31 0,00519 0,00931 0
1 32 0,00044 0,00234 0
1 33 0,00091 -0,00286 0
1 34 0,00717 -0,00682 0
1 35 0,01890 -0,01017 0
1 36 0,03596 -0,01265 0
1 37 0,05827 -0,01425 0
1 38 0,08569 -0,01500 0
1 39 0,11800 -0,01502 0
1 40 0,15490 -0,01441 0
1 41 0,19599 -0,01329 0
1 42 0,24083 -0,01177 0
1 43 0,28892 -0,00998 0
1 44 0,33968 -0,00804 0
1 45 0,39252 -0,00605 0
1 46 0,44679 -0,00410 0
1 47 0,50182 -0,00228 0
1 48 0,55694 -0,00065 0
1 49 0,61147 0,00074 0
1 50 0,66472 0,00186 0
1 51 0,71602 0,00268 0
1 52 0,76475 0,00320 0
1 53 0,81027 0,00342 0
1 54 0,85202 0,00337 0
1 55 0,88944 0,00307 0
1 56 0,92205 0,00258 0
1 57 0,94942 0,00196 0
1 58 0,97118 0,00132 0
1 59 0,98705 0,00071 0
1 60 0,99674 0,00021 0
1 0
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Old   March 29, 2022, 03:17
Default Worked Perfectly for me
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Quote:
Originally Posted by Torchbearer View Post
when u download coordinates from airfoil plotter
you will have repeated coordinates in the excel file , you just need to remove that one repeated co ordinate point , thats simple
Thanks a lot Torchbearer! Saved my day
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Old   October 27, 2022, 06:57
Cool Fix for anyone who tried all the above and none of it worked
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I tried every known solution on the internet, and exactly 0 of them worked.

How I fixed my issue, was:
1. Go to airfoiltools.com and get clark y coordinates
2. On the right hand side of the screen, click "Send to airfoil plotter"
3. On the next screen, choose "CSV file of coordinates"
4. Open the file, create a new z coordinate with 0s
5. Make sure all 3 coordinates have same number of significant digits
6. Convert file to tab delimited (.txt)
7. Open DesignModeler, change units to mm
8. Concept -> 3D curve-> Choose coordinates file.

DONE.

I was struggling with this for days!!! Hope this helps someone else.
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Old   August 28, 2023, 07:50
Default error to coordinates file for blade MH-45
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hello i have same problem for MH-45
Attached Files
File Type: txt mh-45il9.85.txt (1.9 KB, 3 views)
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Old   August 30, 2023, 06:10
Default Naca
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Quote:
Originally Posted by awanerv View Post
Hi all

I have the same error of this topic DS error reading coordinates file.

I dont understand the file NACA-4412 is works fine to import but my other file is get this error.

I search in the CFD forum but nothing can solve my problem here some solution:

The txt file must be saved as ANSI not UNICODE(it saves like that by default)

  • Put comment # at the beginning of each column( such as #x, #y etc)
  • The last row must be 1 0 that means erase the column relative to x,y,z coordinates because they are the same of the first one( I am assuming that you have created an airfoil with closed trailing edge)
  • Save the file as ANSI not unicode.


I dont know where my error in the file Clark Y.txt


I generate from the site aerofoil tools


my ansys version is 17.1, excel version 2013.


I salve the file in txt tab delimited and nothing works.


thanks


Hi there.
Perharps i’m joining the thread a little bit late, but could you explain me how did you make the NACA-4412 archive in more detail? I’ve been struggling with the 3d curve problem for weeks, and knowing how to make propper archives would be really helpful, for I need it for a research proyect.
Thanks!
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