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RAF 30 AIRFOIL (raf30-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAF 30 AIRFOIL (raf30-il)
Reynolds number: 1,000,000
Max Cl/Cd: 71.64 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-raf30-il-1000000-n5.txt
Download as CSV file: xf-raf30-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAF 30 AIRFOIL                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1864   0.10873   0.10565  -0.0119   1.0000   0.0082
 -19.500  -1.2154   0.09996   0.09674  -0.0164   1.0000   0.0081
 -19.250  -1.2405   0.09204   0.08869  -0.0204   1.0000   0.0082
 -19.000  -1.2643   0.08453   0.08105  -0.0242   1.0000   0.0082
 -18.750  -1.2858   0.07749   0.07387  -0.0277   1.0000   0.0082
 -18.500  -1.3027   0.07139   0.06764  -0.0306   1.0000   0.0083
 -18.250  -1.3169   0.06582   0.06194  -0.0333   1.0000   0.0083
 -18.000  -1.3296   0.06067   0.05667  -0.0356   1.0000   0.0083
 -17.750  -1.3375   0.05639   0.05228  -0.0373   1.0000   0.0084
 -17.500  -1.3458   0.05219   0.04797  -0.0390   1.0000   0.0086
 -17.250  -1.3530   0.04833   0.04400  -0.0402   1.0000   0.0087
 -17.000  -1.3582   0.04484   0.04042  -0.0412   1.0000   0.0089
 -16.750  -1.3603   0.04183   0.03731  -0.0419   1.0000   0.0090
 -16.500  -1.3613   0.03906   0.03447  -0.0423   1.0000   0.0093
 -16.250  -1.3602   0.03660   0.03192  -0.0424   1.0000   0.0095
 -16.000  -1.3576   0.03441   0.02965  -0.0424   1.0000   0.0098
 -15.750  -1.3531   0.03249   0.02766  -0.0421   1.0000   0.0101
 -15.500  -1.3482   0.03068   0.02577  -0.0417   1.0000   0.0103
 -15.250  -1.3419   0.02909   0.02410  -0.0410   1.0000   0.0106
 -15.000  -1.3349   0.02764   0.02257  -0.0402   1.0000   0.0109
 -14.750  -1.3272   0.02631   0.02117  -0.0392   1.0000   0.0111
 -14.500  -1.3193   0.02508   0.01988  -0.0380   1.0000   0.0116
 -14.250  -1.3101   0.02402   0.01878  -0.0367   1.0000   0.0120
 -14.000  -1.2999   0.02308   0.01779  -0.0353   1.0000   0.0126
 -13.750  -1.2892   0.02223   0.01689  -0.0337   1.0000   0.0130
 -13.500  -1.2780   0.02147   0.01608  -0.0320   1.0000   0.0135
 -13.250  -1.2664   0.02078   0.01533  -0.0302   1.0000   0.0139
 -13.000  -1.2549   0.02014   0.01464  -0.0281   1.0000   0.0144
 -12.750  -1.2431   0.01956   0.01403  -0.0260   1.0000   0.0149
 -12.500  -1.2300   0.01909   0.01356  -0.0239   1.0000   0.0157
 -12.250  -1.2181   0.01864   0.01306  -0.0214   1.0000   0.0163
 -12.000  -1.2061   0.01822   0.01262  -0.0188   1.0000   0.0168
 -11.750  -1.1919   0.01782   0.01217  -0.0167   1.0000   0.0174
 -11.500  -1.1756   0.01741   0.01172  -0.0148   1.0000   0.0178
 -11.250  -1.1602   0.01695   0.01123  -0.0128   1.0000   0.0183
 -11.000  -1.1438   0.01654   0.01079  -0.0110   1.0000   0.0189
 -10.750  -1.1264   0.01617   0.01041  -0.0093   1.0000   0.0195
 -10.500  -1.1086   0.01582   0.01005  -0.0076   1.0000   0.0202
 -10.250  -1.0900   0.01552   0.00972  -0.0060   1.0000   0.0209
 -10.000  -1.0713   0.01522   0.00939  -0.0044   1.0000   0.0215
  -9.750  -1.0526   0.01492   0.00906  -0.0028   1.0000   0.0219
  -9.500  -1.0338   0.01462   0.00873  -0.0012   1.0000   0.0222
  -9.250  -1.0156   0.01429   0.00837   0.0005   1.0000   0.0227
  -9.000  -0.9894   0.01381   0.00788   0.0004   0.9990   0.0237
  -8.750  -0.9583   0.01342   0.00747  -0.0006   0.9969   0.0245
  -8.250  -0.8984   0.01275   0.00677  -0.0021   0.9907   0.0260
  -8.000  -0.8684   0.01243   0.00643  -0.0028   0.9867   0.0267
  -7.750  -0.8377   0.01214   0.00612  -0.0037   0.9826   0.0273
  -7.500  -0.8098   0.01186   0.00581  -0.0038   0.9759   0.0277
  -7.250  -0.7788   0.01153   0.00546  -0.0047   0.9697   0.0284
  -7.000  -0.7457   0.01116   0.00508  -0.0060   0.9622   0.0296
  -6.750  -0.7076   0.01082   0.00473  -0.0085   0.9545   0.0307
  -6.500  -0.6665   0.01050   0.00440  -0.0116   0.9440   0.0319
  -6.250  -0.6259   0.01021   0.00408  -0.0145   0.9278   0.0333
  -6.000  -0.5922   0.01002   0.00381  -0.0158   0.9056   0.0344
  -5.750  -0.5654   0.00986   0.00357  -0.0156   0.8835   0.0367
  -5.500  -0.5409   0.00969   0.00336  -0.0149   0.8646   0.0404
  -5.250  -0.5175   0.00948   0.00313  -0.0140   0.8476   0.0496
  -5.000  -0.4957   0.00915   0.00288  -0.0129   0.8316   0.0757
  -4.750  -0.4724   0.00892   0.00269  -0.0120   0.8175   0.0945
  -4.500  -0.4480   0.00875   0.00253  -0.0113   0.8040   0.1074
  -4.250  -0.4240   0.00855   0.00236  -0.0105   0.7907   0.1253
  -4.000  -0.4006   0.00829   0.00218  -0.0097   0.7781   0.1517
  -3.750  -0.3769   0.00806   0.00202  -0.0089   0.7657   0.1787
  -3.500  -0.3533   0.00782   0.00187  -0.0080   0.7534   0.2102
  -3.250  -0.3291   0.00762   0.00174  -0.0073   0.7393   0.2396
  -3.000  -0.3051   0.00747   0.00163  -0.0065   0.7213   0.2677
  -2.750  -0.2805   0.00735   0.00153  -0.0058   0.7019   0.2912
  -2.500  -0.2556   0.00723   0.00144  -0.0052   0.6860   0.3128
  -2.000  -0.2046   0.00701   0.00128  -0.0042   0.6616   0.3567
  -1.750  -0.1797   0.00685   0.00121  -0.0035   0.6506   0.3888
  -1.500  -0.1558   0.00663   0.00114  -0.0028   0.6396   0.4364
  -1.250  -0.1310   0.00647   0.00109  -0.0021   0.6289   0.4761
  -1.000  -0.1056   0.00636   0.00106  -0.0015   0.6185   0.5070
  -0.500  -0.0535   0.00625   0.00103  -0.0006   0.5968   0.5501
  -0.250  -0.0267   0.00624   0.00102  -0.0003   0.5866   0.5634
   0.000   0.0000   0.00624   0.00102   0.0000   0.5753   0.5756
   0.250   0.0267   0.00624   0.00102   0.0003   0.5632   0.5866
   0.500   0.0534   0.00626   0.00103   0.0007   0.5481   0.5963
   0.750   0.0797   0.00631   0.00104   0.0011   0.5302   0.6078
   1.000   0.1056   0.00636   0.00106   0.0015   0.5070   0.6184
   1.250   0.1310   0.00647   0.00109   0.0021   0.4763   0.6287
   1.500   0.1556   0.00664   0.00114   0.0028   0.4341   0.6398
   1.750   0.1797   0.00684   0.00121   0.0035   0.3893   0.6504
   2.000   0.2046   0.00701   0.00128   0.0041   0.3564   0.6613
   2.500   0.2556   0.00723   0.00144   0.0052   0.3127   0.6860
   2.750   0.2805   0.00735   0.00153   0.0058   0.2916   0.7021
   3.000   0.3050   0.00747   0.00163   0.0065   0.2672   0.7216
   3.250   0.3290   0.00763   0.00175   0.0073   0.2380   0.7391
   3.500   0.3532   0.00783   0.00187   0.0080   0.2097   0.7533
   3.750   0.3768   0.00806   0.00202   0.0089   0.1778   0.7658
   4.000   0.4005   0.00829   0.00218   0.0097   0.1514   0.7785
   4.250   0.4239   0.00855   0.00237   0.0106   0.1244   0.7909
   4.500   0.4480   0.00875   0.00253   0.0113   0.1072   0.8038
   4.750   0.4723   0.00892   0.00269   0.0120   0.0939   0.8172
   5.000   0.4955   0.00915   0.00288   0.0129   0.0750   0.8318
   5.250   0.5173   0.00949   0.00314   0.0141   0.0484   0.8475
   5.500   0.5409   0.00969   0.00336   0.0149   0.0402   0.8648
   5.750   0.5654   0.00985   0.00357   0.0156   0.0368   0.8835
   6.000   0.5922   0.01002   0.00381   0.0158   0.0343   0.9057
   6.250   0.6261   0.01022   0.00408   0.0145   0.0332   0.9282
   6.500   0.6663   0.01050   0.00440   0.0116   0.0319   0.9440
   6.750   0.7074   0.01083   0.00474   0.0085   0.0307   0.9544
   7.000   0.7454   0.01115   0.00507   0.0061   0.0297   0.9620
   7.250   0.7788   0.01153   0.00546   0.0047   0.0285   0.9697
   7.500   0.8098   0.01186   0.00581   0.0038   0.0277   0.9759
   7.750   0.8376   0.01214   0.00612   0.0037   0.0273   0.9826
   8.000   0.8682   0.01243   0.00644   0.0029   0.0267   0.9867
   8.250   0.8983   0.01275   0.00677   0.0022   0.0260   0.9906
   8.750   0.9584   0.01342   0.00748   0.0006   0.0245   0.9969
   9.000   0.9893   0.01381   0.00786  -0.0004   0.0236   0.9989
   9.250   1.0158   0.01428   0.00836  -0.0005   0.0227   1.0000
   9.500   1.0339   0.01463   0.00873   0.0012   0.0223   1.0000
   9.750   1.0530   0.01490   0.00904   0.0028   0.0219   1.0000
  10.000   1.0715   0.01521   0.00938   0.0044   0.0215   1.0000
  10.250   1.0898   0.01554   0.00975   0.0061   0.0210   1.0000
  10.500   1.1082   0.01586   0.01009   0.0077   0.0203   1.0000
  10.750   1.1261   0.01619   0.01044   0.0093   0.0197   1.0000
  11.000   1.1437   0.01655   0.01081   0.0110   0.0190   1.0000
  11.250   1.1604   0.01695   0.01122   0.0128   0.0183   1.0000
  11.500   1.1757   0.01740   0.01171   0.0148   0.0178   1.0000
  11.750   1.1921   0.01781   0.01216   0.0166   0.0173   1.0000
  12.000   1.2061   0.01822   0.01261   0.0188   0.0168   1.0000
  12.250   1.2185   0.01861   0.01303   0.0214   0.0162   1.0000
  12.500   1.2309   0.01905   0.01350   0.0237   0.0155   1.0000
  12.750   1.2432   0.01955   0.01402   0.0260   0.0149   1.0000
  13.000   1.2549   0.02014   0.01463   0.0281   0.0142   1.0000
  13.250   1.2667   0.02077   0.01531   0.0301   0.0138   1.0000
  13.500   1.2784   0.02146   0.01606   0.0320   0.0135   1.0000
  13.750   1.2896   0.02222   0.01687   0.0337   0.0130   1.0000
  14.000   1.3003   0.02306   0.01777   0.0353   0.0126   1.0000
  14.250   1.3105   0.02400   0.01876   0.0367   0.0120   1.0000
  14.500   1.3196   0.02507   0.01987   0.0380   0.0115   1.0000
  14.750   1.3277   0.02629   0.02115   0.0392   0.0112   1.0000
  15.000   1.3352   0.02763   0.02256   0.0402   0.0108   1.0000
  15.250   1.3430   0.02902   0.02402   0.0410   0.0105   1.0000
  15.500   1.3487   0.03066   0.02575   0.0416   0.0104   1.0000
  15.750   1.3541   0.03243   0.02759   0.0421   0.0101   1.0000
  16.000   1.3585   0.03437   0.02960   0.0423   0.0097   1.0000
  16.250   1.3613   0.03654   0.03186   0.0423   0.0095   1.0000
  16.500   1.3622   0.03903   0.03443   0.0422   0.0092   1.0000
  16.750   1.3616   0.04177   0.03725   0.0417   0.0090   1.0000
  17.000   1.3592   0.04481   0.04039   0.0411   0.0088   1.0000
  17.250   1.3543   0.04828   0.04396   0.0401   0.0087   1.0000
  17.500   1.3468   0.05220   0.04798   0.0388   0.0086   1.0000
  17.750   1.3399   0.05620   0.05209   0.0372   0.0084   1.0000
  18.000   1.3301   0.06076   0.05677   0.0353   0.0084   1.0000
  18.250   1.3185   0.06577   0.06190   0.0331   0.0083   1.0000
  18.500   1.3051   0.07122   0.06747   0.0305   0.0083   1.0000
  18.750   1.2891   0.07719   0.07357   0.0276   0.0082   1.0000
  19.000   1.2667   0.08437   0.08089   0.0240   0.0082   1.0000
  19.250   1.2442   0.09169   0.08834   0.0203   0.0081   1.0000
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