dae11.dat

一个可以生成标准翼型坐标

% DAE 11 Daedalus Airfoil 
% from Mark Drela
     42.       40.
%     X/C       Y/C  
% upper surface  
0.000000  0.000000   
0.000883  0.005097  
0.003417  0.011421
0.008417  0.019287   
0.016619  0.028679   
0.028485  0.039251   
0.044085  0.050490   
0.062995  0.061754   
0.084520  0.072514   
0.108024  0.082466   
0.133039  0.091476   
0.159197  0.099489   
0.186216  0.106500   
0.213885  0.112508   
0.242030  0.117536   
0.270512  0.121609   
0.299232  0.124754   
0.328135  0.126996   
0.357167  0.128336   
0.386255  0.128806   
0.415323  0.128391   
0.444338  0.127068   
0.473284  0.124848   
0.502104  0.121740   
0.530735  0.117738   
0.559192  0.112804   
0.587628  0.106875   
0.616310  0.099961   
0.645478  0.092177   
0.675260  0.083695   
0.705687  0.074715   
0.736634  0.065482   
0.767378  0.056399   
0.797803  0.047590   
0.827970  0.039139   
0.857968  0.031118   
0.887980  0.023556   
0.918618  0.016374   
0.947881  0.010041   
0.970011  0.005613   
0.986485  0.002537   
1.000000  0.000000      
%X/C       Y/C    
%lower surface   
0.000000  0.000000   
0.000626 -0.003555   
0.002138 -0.006473   
0.004541 -0.008835   
0.008212 -0.010744   
0.014240 -0.012418   
0.024697 -0.013921   
0.041573 -0.014931   
0.065014 -0.015107   
0.092723 -0.014502   
0.122696 -0.013331   
0.153786 -0.011784   
0.185487 -0.010003   
0.217549 -0.008087   
0.249834 -0.006102   
0.282263 -0.004093   
0.314698 -0.002099   
0.347047 -0.000149   
0.379318  0.001724   
0.411508  0.003509   
0.443624  0.005174   
0.475671  0.006709   
0.507637  0.008092   
0.539527  0.009282   
0.571366  0.010264   
0.603162  0.011026   
0.634928  0.011552   
0.666677  0.011849   
0.698414  0.011916   
0.730135  0.011759   
0.761819  0.011381   
0.793447  0.010763   
0.825020  0.009891   
0.856580  0.008751   
0.888343  0.007325   
0.920025  0.005610   
0.948000  0.003865   
0.969655  0.002348   
0.986285  0.001076   
1.000000  0.000000