Airfoil coordinates into Profili software
#1
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Airfoil coordinates into Profili software
I want to cut a foam wing with this coordinates but I don´t know hot to put it into Profili software. Can someone help me with that.
Thanks
Marco Vergara
S8064
1.000000 0.000000
0.997927 0.000125
0.991844 0.000661
0.981950 0.001759
0.968438 0.003565
0.951588 0.006193
0.931716 0.009686
0.909164 0.014035
0.884293 0.019168
0.857469 0.024954
0.829053 0.031198
0.799390 0.037630
0.768826 0.043760
0.737098 0.049161
0.703928 0.053909
0.669588 0.058180
0.634301 0.061961
0.598271 0.065229
0.561701 0.067947
0.524799 0.070079
0.487769 0.071601
0.450799 0.072500
0.414069 0.072755
0.377770 0.072374
0.342087 0.071387
0.307218 0.069831
0.273369 0.067736
0.240738 0.065134
0.209521 0.062054
0.179900 0.058531
0.152050 0.054600
0.126136 0.050302
0.102312 0.045678
0.080718 0.040772
0.061481 0.035636
0.044723 0.030322
0.030576 0.024873
0.019091 0.019310
0.010271 0.013670
0.004145 0.008047
0.000637 0.002692
0.000328 -0.001911
0.003568 -0.006325
0.009851 -0.011082
0.018933 -0.015812
0.030792 -0.020402
0.045404 -0.024768
0.062686 -0.028860
0.082555 -0.032657
0.104908 -0.036143
0.129620 -0.039299
0.156536 -0.042118
0.185485 -0.044585
0.216282 -0.046683
0.248732 -0.048388
0.282633 -0.049680
0.317775 -0.050530
0.353959 -0.050905
0.390991 -0.050795
0.428663 -0.050184
0.466779 -0.049071
0.505162 -0.047491
0.543597 -0.045496
0.581815 -0.043133
0.619551 -0.040409
0.656518 -0.037280
0.692670 -0.033539
0.728117 -0.029328
0.762681 -0.025064
0.796024 -0.020943
0.827817 -0.017097
0.857738 -0.013617
0.885475 -0.010558
0.910730 -0.007944
0.933228 -0.005769
0.952715 -0.003991
0.969006 -0.002502
0.982067 -0.001257
0.991810 -0.000404
0.997911 -0.000042
1.000000 0.000000
Thanks
Marco Vergara
S8064
1.000000 0.000000
0.997927 0.000125
0.991844 0.000661
0.981950 0.001759
0.968438 0.003565
0.951588 0.006193
0.931716 0.009686
0.909164 0.014035
0.884293 0.019168
0.857469 0.024954
0.829053 0.031198
0.799390 0.037630
0.768826 0.043760
0.737098 0.049161
0.703928 0.053909
0.669588 0.058180
0.634301 0.061961
0.598271 0.065229
0.561701 0.067947
0.524799 0.070079
0.487769 0.071601
0.450799 0.072500
0.414069 0.072755
0.377770 0.072374
0.342087 0.071387
0.307218 0.069831
0.273369 0.067736
0.240738 0.065134
0.209521 0.062054
0.179900 0.058531
0.152050 0.054600
0.126136 0.050302
0.102312 0.045678
0.080718 0.040772
0.061481 0.035636
0.044723 0.030322
0.030576 0.024873
0.019091 0.019310
0.010271 0.013670
0.004145 0.008047
0.000637 0.002692
0.000328 -0.001911
0.003568 -0.006325
0.009851 -0.011082
0.018933 -0.015812
0.030792 -0.020402
0.045404 -0.024768
0.062686 -0.028860
0.082555 -0.032657
0.104908 -0.036143
0.129620 -0.039299
0.156536 -0.042118
0.185485 -0.044585
0.216282 -0.046683
0.248732 -0.048388
0.282633 -0.049680
0.317775 -0.050530
0.353959 -0.050905
0.390991 -0.050795
0.428663 -0.050184
0.466779 -0.049071
0.505162 -0.047491
0.543597 -0.045496
0.581815 -0.043133
0.619551 -0.040409
0.656518 -0.037280
0.692670 -0.033539
0.728117 -0.029328
0.762681 -0.025064
0.796024 -0.020943
0.827817 -0.017097
0.857738 -0.013617
0.885475 -0.010558
0.910730 -0.007944
0.933228 -0.005769
0.952715 -0.003991
0.969006 -0.002502
0.982067 -0.001257
0.991810 -0.000404
0.997911 -0.000042
1.000000 0.000000
#2
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RE: Airfoil coordinates into Profili software
Hi
Not sure how to in profili but I can pu them into compufoil then export it as a dxf file if that helps at all
Thanks
Troy
Not sure how to in profili but I can pu them into compufoil then export it as a dxf file if that helps at all
Thanks
Troy
#3
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RE: Airfoil coordinates into Profili software
Hi Troy, I am planing to cut this airfoil in my cnc foam cutter, I need a .PRO .DAT .COR OR .KOO archive. Can Compufoil export it in one of this archives? if not is OK, it would be easier to convert a DXF file.
Thank you for your help in advance
Marco
Thank you for your help in advance
Marco
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RE: Airfoil coordinates into Profili software
Marco,
1) create a file with Notepad and name it S8064.DAT
2) Paste the airfoil coordinates as you did hereabove
3) Save your file --> at this point you have a DAT file compatible with Profili
4) In Profili, Go to the menu --> Airfoils --> Airfoil Management --> Import --> Import Airfoil from a .DAT file
That's it !
If you have difficulties to create the .DAT file then drop a PM with your Email address and I'll reply with the file.
Cheers,
Bernard
1) create a file with Notepad and name it S8064.DAT
2) Paste the airfoil coordinates as you did hereabove
3) Save your file --> at this point you have a DAT file compatible with Profili
4) In Profili, Go to the menu --> Airfoils --> Airfoil Management --> Import --> Import Airfoil from a .DAT file
That's it !
If you have difficulties to create the .DAT file then drop a PM with your Email address and I'll reply with the file.
Cheers,
Bernard
#5
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RE: Airfoil coordinates into Profili software
Hi Bernard,
I send you a pm with my e mail address. I tried to import the dat file into Profili but I got a message: name the airfoil
and didn´t find the way to do it.
Thank you for your help
Marco
I send you a pm with my e mail address. I tried to import the dat file into Profili but I got a message: name the airfoil
and didn´t find the way to do it.
Thank you for your help
Marco
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RE: Airfoil coordinates into Profili software
Troy: it works thank you for your help.
Bob: I use Profili 2.19 too but the s8036 is a diferent airfoil, s8064 is an airfoil designed by Michel Selig for Q500 racing airplanes.
Thank you
Bob: I use Profili 2.19 too but the s8036 is a diferent airfoil, s8064 is an airfoil designed by Michel Selig for Q500 racing airplanes.
Thank you
#10
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RE: Airfoil coordinates into Profili software
Take a look at [link=http://www.tdmsoftware.com/afd]Airfoil Design Workshop[/link]
You can provide airfoil coordinates as a text file and then view, display, modify and output as a DXF file.
Also imports .DAT file formates.
You can provide airfoil coordinates as a text file and then view, display, modify and output as a DXF file.
Also imports .DAT file formates.
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ask a question
Please tell me about it ,i am a student ,i do some research on airfoil design.
thanks very much.