[WWI] Airfoil Needed

[Chris Banyai-Riepl]

Try these for plot ordinates:

X             Y

 1.00000       0.00000
 0.94801       0.01901
 0.89900       0.02819
 0.85274       0.03651
 0.80903       0.04365
 0.76769       0.04904
 0.72855       0.05326
 0.69146       0.05686
 0.65627       0.06023
 0.62287       0.06316
 0.59112       0.06565
 0.56094       0.06770
 0.53220       0.06940
 0.50483       0.07078
 0.47874       0.07184
 0.45384       0.07267
 0.43007       0.07333
 0.40737       0.07385
 0.38566       0.07435
 0.36489       0.07481
 0.34501       0.07519
 0.32596       0.07550
 0.30771       0.07573
 0.29020       0.07592
 0.27340       0.07606
 0.25728       0.07611
 0.24178       0.07606
 0.22689       0.07588
 0.21257       0.07559
 0.19879       0.07515
 0.18552       0.07456
 0.17275       0.07382
 0.16044       0.07292
 0.14858       0.07184
 0.13713       0.07047
 0.12610       0.06895
 0.11544       0.06732
 0.10515       0.06560
 0.09521       0.06390
 0.08561       0.06217
 0.07633       0.06029
 0.06735       0.05817
 0.05866       0.05579
 0.05026       0.05309
 0.04212       0.04977
 0.03424       0.04603
 0.02660       0.04192
 0.01920       0.03779
 0.01203       0.03259
 0.00508       0.02395
 0.00168       0.01518
 0.00000       0.00000
 0.00000       0.00000
 0.00168      -0.00039
 0.00508      -0.00039
 0.01203      -0.00003
 0.01920       0.00050
 0.02660       0.00115
 0.03424       0.00192
 0.04212       0.00272
 0.05026       0.00352
 0.05866       0.00430
 0.06735       0.00506
 0.07633       0.00581
 0.08561       0.00655
 0.09521       0.00727
 0.10515       0.00795
 0.11544       0.00859
 0.12610       0.00916
 0.13713       0.00962
 0.14858       0.00997
 0.16044       0.01002
 0.17275       0.00994
 0.18552       0.00977
 0.19879       0.00952
 0.21257       0.00938
 0.22689       0.00925
 0.24178       0.00911
 0.25728       0.00896
 0.27340       0.00880
 0.29020       0.00861
 0.30771       0.00839
 0.32596       0.00813
 0.34501       0.00785
 0.36489       0.00754
 0.38566       0.00722
 0.40737       0.00691
 0.43007       0.00661
 0.45384       0.00627
 0.47874       0.00588
 0.50483       0.00538
 0.53220       0.00467
 0.56094       0.00393
 0.59112       0.00320
 0.62287       0.00269
 0.65627       0.00230
 0.69146       0.00190
 0.72855       0.00123
 0.76769       0.00048
 0.80903      -0.00004
 0.85274      -0.00008
 0.89900       0.00000
 0.94801       0.00000
 1.00000       0.00000 

> -----Original Message-----
> From: wwi-bounces at wwi-models.org 
> [mailto:wwi-bounces at wwi-models.org] On Behalf Of joe huntley
> Sent: Friday, September 14, 2007 2:10 PM
> To: World War I Modeling Mailing List
> Subject: Re: [WWI] Airfoil Needed
> 
> program says its missing a coordinate
> 
> ----- Original Message -----
> From: "ernest thomas" <reason108 at hotmail.com>
> To: <wwi at wwi-models.org>
> Sent: Friday, September 14, 2007 3:54 PM
> Subject: Re: [WWI] Airfoil Needed
> 
> 
> > Damn!
> >
> >>From: "Chris Banyai-Riepl" >
> >>Sorry E, you lose.
> >
> > _________________________________________________________________
> > Get a FREE small business Web site and more from MicrosoftR 
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> > http://clk.atdmt.com/MRT/go/aub0930003811mrt/direct/01/
> > 
> 
>