Marco Vergara

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

troyhm

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

Marco Vergara

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

bbt

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

Marco Vergara

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

troyhm

Hi Macro

Here is the file, just rename it to .cor and it will work

Thanks

Troy

N1EDM

My Feedback: (2)

I have Profili 2.19. I looked at Airfoils --> Airfoil Management and found the S8036 already listed there.

Does this help????

Bob

Marco Vergara

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

N1EDM

My Feedback: (2)

Sorry Marco, my mistake....

Bob

orectolobus

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.

FLYPENG

Hello, I import your txt file sucessful by Profili, rename its name ,so I want to know how did you create the txt file.
Please tell me about it ,i am a student ,i do some research on airfoil design.
thanks very much.

FLYPENG