DAE-11 AIRFOIL 1.000000 0.000000 0.986483 0.002538 0.970008 0.005615 0.947875 0.010045 0.918609 0.016380 0.887967 0.023564 0.857951 0.031128 0.827950 0.039152 0.797780 0.047605 0.767351 0.056417 0.736604 0.065502 0.705653 0.074738 0.675223 0.083720 0.645437 0.092205 0.616266 0.099991 0.587581 0.106907 0.559141 0.112838 0.530681 0.117774 0.502047 0.121778 0.473223 0.124888 0.444274 0.127109 0.415255 0.128434 0.386183 0.128850 0.357092 0.128382 0.328056 0.127043 0.299149 0.124802 0.270425 0.121658 0.241940 0.117585 0.213791 0.112558 0.186118 0.106551 0.159095 0.099540 0.132934 0.091527 0.107915 0.082517 0.084408 0.072565 0.062879 0.061804 0.043966 0.050540 0.028364 0.039300 0.016496 0.028727 0.008293 0.019335 0.003292 0.011468 0.000757 0.005143 0.000000 0.000000 0.000492 -0.003486 0.002012 -0.006428 0.004415 -0.008791 0.008086 -0.010700 0.014115 -0.012375 0.024573 -0.013878 0.041451 -0.014889 0.064895 -0.015066 0.092608 -0.014462 0.122584 -0.013293 0.153678 -0.011747 0.185384 -0.009967 0.217450 -0.008052 0.249739 -0.006069 0.282172 -0.004061 0.314611 -0.002068 0.346965 -0.000119 0.379240 0.001752 0.411434 0.003536 0.443554 0.005200 0.475605 0.006734 0.507575 0.008115 0.539469 0.009304 0.571312 0.010285 0.603112 0.011045 0.634882 0.011570 0.666635 0.011866 0.698376 0.011931 0.730101 0.011773 0.761789 0.011393 0.793421 0.010774 0.824998 0.009900 0.856562 0.008759 0.888329 0.007331 0.920015 0.005614 0.947994 0.003868 0.969651 0.002350 0.986283 0.001077 1.000000 0.000000