NASA/LANGLEY RC-08(N)1 AIRFOIL
       42.       42.

  0.000000  0.000000
  0.000807  0.002964
  0.003351  0.006415
  0.009719  0.011533
  0.023228  0.018503
  0.048001  0.026872
  0.073484  0.032934
  0.098564  0.037575
  0.123687  0.041366
  0.148872  0.044607
  0.174090  0.047318
  0.199390  0.049550
  0.224642  0.051341
  0.249806  0.052722
  0.300098  0.054474
  0.350365  0.055035
  0.375496  0.054896
  0.400597  0.054487
  0.425700  0.053778
  0.450805  0.052778
  0.475880  0.051469
  0.500927  0.049879
  0.525976  0.048020
  0.551015  0.045920
  0.576025  0.043601
  0.601056  0.041051
  0.626098  0.038291
  0.651131  0.035342
  0.676175  0.032232
  0.701139  0.029012
  0.726013  0.025752
  0.750967  0.022542
  0.775830  0.019462
  0.800543  0.016591
  0.825325  0.013920
  0.850165  0.011449
  0.875045  0.009159
  0.899995  0.007049
  0.924973  0.005129
  0.949940  0.003399
  0.974917  0.001879
  1.000000  0.000640

  0.000000  0.000000
  0.004201 -0.004831
  0.006645 -0.005691
  0.015258 -0.006543
  0.026727 -0.008572
  0.051926 -0.010491
  0.076423 -0.012173
  0.101330 -0.013833
  0.126187 -0.015414
  0.150993 -0.016854
  0.175769 -0.018175
  0.200464 -0.019396
  0.225209 -0.020527
  0.250044 -0.021587
  0.299741 -0.023398
  0.349477 -0.024759
  0.374349 -0.025249
  0.399251 -0.025600
  0.424162 -0.025800
  0.449051 -0.025830
  0.473981 -0.025680
  0.498929 -0.025360
  0.523897 -0.024870
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  0.573851 -0.023480
  0.598827 -0.022619
  0.623793 -0.021709
  0.648768 -0.020769
  0.673734 -0.019859
  0.698781 -0.019019
  0.723917 -0.018258
  0.748964 -0.017527
  0.774110 -0.016766
  0.799406 -0.015845
  0.824631 -0.014673
  0.849804 -0.013222
  0.874917 -0.011532
  0.899958 -0.009681
  0.924990 -0.007761
  0.950011 -0.005781
  0.975041 -0.003600
  1.000000 -0.000640