OGRID TEST NACA 0012 AIRFOIL
YSYM      FNU       FNL
1.0       33        33   81    31
   X          Y
0.0          0.0
 0.0050     .01153
  .0125     .01894
  .0250     .02615
  .0500     .03555
  .0750     .04200
  .1000     .04683
  .1500     .05345
  .2000     .05737
  .2500     .05941
  .2600     .05962
  .2700     .05978
  .2800     .05992
  .2900     .05999
  .3000     .06000
  .3100     .05999
  .3200     .05992
  .3300     .05980
  .3400     .05965
  .3500     .05947
  .4000     .05803
  .4500     .05581
  .5000     .05294
  .5500     .04952
  .6000     .04563
  .6500     .04137
  .7000     .03664
  .7500     .03161
  .8000     .02623
  .8500     .02055
  .9000     .01448
  .9500     .00807
 1.0000     .00126
XSING
.01   0.0