RUTAN WING AIRFOIL (amsoil2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: RUTAN WING AIRFOIL (amsoil2-il) Reynolds number: 1,000,000 Max Cl/Cd: 74.91 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-amsoil2-il-1000000.txt Download as CSV file: xf-amsoil2-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: RUTAN WING 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -1.1889 0.09296 0.09032 -0.0170 1.0000 0.0198
-17.500 -1.2567 0.07521 0.07228 -0.0285 1.0000 0.0197
-17.250 -1.2924 0.06449 0.06134 -0.0358 1.0000 0.0197
-17.000 -1.3144 0.05718 0.05385 -0.0405 1.0000 0.0197
-16.750 -1.3288 0.05164 0.04815 -0.0435 1.0000 0.0198
-16.500 -1.3379 0.04729 0.04365 -0.0455 1.0000 0.0199
-16.250 -1.3428 0.04373 0.03995 -0.0467 1.0000 0.0200
-16.000 -1.3446 0.04076 0.03685 -0.0474 1.0000 0.0201
-15.750 -1.3434 0.03826 0.03422 -0.0476 1.0000 0.0203
-15.500 -1.3396 0.03617 0.03202 -0.0475 1.0000 0.0204
-15.250 -1.3475 0.03310 0.02880 -0.0468 1.0000 0.0206
-15.000 -1.3478 0.03093 0.02652 -0.0458 1.0000 0.0209
-14.750 -1.3424 0.02936 0.02488 -0.0447 1.0000 0.0211
-14.500 -1.3337 0.02815 0.02361 -0.0435 1.0000 0.0213
-14.250 -1.3233 0.02714 0.02254 -0.0421 1.0000 0.0216
-14.000 -1.3121 0.02626 0.02159 -0.0405 1.0000 0.0218
-13.750 -1.2982 0.02546 0.02073 -0.0392 1.0000 0.0221
-13.500 -1.2816 0.02466 0.01986 -0.0382 1.0000 0.0224
-13.250 -1.2636 0.02390 0.01903 -0.0373 1.0000 0.0228
-13.000 -1.2442 0.02322 0.01827 -0.0366 1.0000 0.0231
-12.750 -1.2236 0.02261 0.01757 -0.0360 1.0000 0.0235
-12.500 -1.2017 0.02210 0.01698 -0.0354 1.0000 0.0237
-12.250 -1.1863 0.02074 0.01555 -0.0343 1.0000 0.0243
-12.000 -1.1652 0.02004 0.01482 -0.0338 1.0000 0.0247
-11.750 -1.1424 0.01950 0.01426 -0.0334 1.0000 0.0252
-11.500 -1.1189 0.01899 0.01372 -0.0331 1.0000 0.0256
-11.250 -1.0951 0.01849 0.01317 -0.0327 1.0000 0.0261
-11.000 -1.0708 0.01800 0.01263 -0.0325 1.0000 0.0266
-10.750 -1.0460 0.01755 0.01212 -0.0323 1.0000 0.0271
-10.500 -1.0206 0.01718 0.01169 -0.0321 1.0000 0.0274
-10.250 -0.9990 0.01624 0.01073 -0.0317 1.0000 0.0283
-10.000 -0.9691 0.01577 0.01026 -0.0326 0.9927 0.0290
-9.750 -0.9378 0.01539 0.00985 -0.0337 0.9837 0.0297
-9.500 -0.9093 0.01502 0.00944 -0.0340 0.9732 0.0304
-9.250 -0.8842 0.01470 0.00906 -0.0336 0.9621 0.0310
-9.000 -0.8600 0.01444 0.00873 -0.0329 0.9521 0.0315
-8.750 -0.8386 0.01382 0.00806 -0.0318 0.9427 0.0323
-8.500 -0.8141 0.01342 0.00765 -0.0313 0.9345 0.0332
-8.250 -0.7894 0.01315 0.00734 -0.0307 0.9270 0.0340
-8.000 -0.7631 0.01289 0.00705 -0.0305 0.9204 0.0349
-7.750 -0.7370 0.01264 0.00675 -0.0302 0.9138 0.0357
-7.500 -0.7110 0.01236 0.00641 -0.0298 0.9077 0.0364
-7.250 -0.6853 0.01187 0.00591 -0.0296 0.9015 0.0376
-7.000 -0.6589 0.01161 0.00563 -0.0294 0.8954 0.0387
-6.750 -0.6318 0.01140 0.00539 -0.0292 0.8900 0.0399
-6.500 -0.6041 0.01119 0.00515 -0.0292 0.8847 0.0409
-6.250 -0.5773 0.01085 0.00478 -0.0290 0.8793 0.0423
-6.000 -0.5504 0.01060 0.00452 -0.0289 0.8740 0.0439
-5.750 -0.5222 0.01039 0.00431 -0.0289 0.8693 0.0455
-5.500 -0.4941 0.01023 0.00412 -0.0290 0.8640 0.0469
-5.250 -0.4669 0.00993 0.00382 -0.0289 0.8587 0.0494
-5.000 -0.4388 0.00975 0.00364 -0.0289 0.8536 0.0517
-4.750 -0.4104 0.00957 0.00344 -0.0290 0.8484 0.0541
-4.500 -0.3824 0.00935 0.00325 -0.0290 0.8432 0.0579
-4.250 -0.3542 0.00922 0.00309 -0.0290 0.8383 0.0613
-4.000 -0.3257 0.00901 0.00293 -0.0291 0.8339 0.0662
-3.750 -0.2970 0.00885 0.00277 -0.0293 0.8290 0.0711
-3.500 -0.2685 0.00870 0.00265 -0.0294 0.8243 0.0766
-3.250 -0.2400 0.00857 0.00251 -0.0294 0.8195 0.0831
-3.000 -0.2109 0.00843 0.00241 -0.0297 0.8156 0.0889
-2.750 -0.1821 0.00826 0.00229 -0.0298 0.8111 0.0979
-2.500 -0.1533 0.00811 0.00218 -0.0300 0.8065 0.1086
-2.250 -0.1247 0.00799 0.00209 -0.0301 0.8017 0.1229
-2.000 -0.0956 0.00781 0.00201 -0.0304 0.7977 0.1424
-1.750 -0.0667 0.00759 0.00192 -0.0306 0.7934 0.1732
-1.500 -0.0381 0.00729 0.00182 -0.0309 0.7890 0.2297
-1.250 -0.0109 0.00659 0.00164 -0.0312 0.7838 0.3864
-1.000 0.0163 0.00579 0.00151 -0.0314 0.7766 0.5754
-0.750 0.0446 0.00557 0.00149 -0.0314 0.7679 0.6449
-0.500 0.0736 0.00547 0.00148 -0.0315 0.7586 0.6790
-0.250 0.1023 0.00544 0.00146 -0.0315 0.7468 0.7046
0.000 0.1315 0.00539 0.00147 -0.0316 0.7370 0.7249
0.250 0.1604 0.00539 0.00148 -0.0316 0.7280 0.7424
0.500 0.1897 0.00538 0.00150 -0.0317 0.7188 0.7556
0.750 0.2189 0.00541 0.00151 -0.0318 0.7074 0.7679
1.000 0.2476 0.00544 0.00153 -0.0318 0.6903 0.7803
1.250 0.2763 0.00549 0.00155 -0.0318 0.6674 0.7911
1.500 0.3048 0.00561 0.00158 -0.0318 0.6396 0.8030
1.750 0.3324 0.00575 0.00165 -0.0315 0.6013 0.8167
2.000 0.3590 0.00614 0.00175 -0.0313 0.5226 0.8250
2.250 0.3821 0.00715 0.00207 -0.0309 0.3448 0.8312
2.500 0.4063 0.00801 0.00238 -0.0306 0.2121 0.8374
2.750 0.4331 0.00837 0.00255 -0.0305 0.1653 0.8434
3.000 0.4603 0.00861 0.00270 -0.0304 0.1393 0.8502
3.250 0.4880 0.00885 0.00285 -0.0304 0.1201 0.8569
3.500 0.5152 0.00906 0.00300 -0.0302 0.1049 0.8632
3.750 0.5426 0.00925 0.00315 -0.0301 0.0941 0.8697
4.500 0.6243 0.00983 0.00366 -0.0297 0.0745 0.8902
4.750 0.6507 0.01007 0.00388 -0.0294 0.0691 0.8973
5.000 0.6775 0.01021 0.00405 -0.0291 0.0662 0.9050
5.250 0.7037 0.01045 0.00426 -0.0288 0.0623 0.9128
5.500 0.7294 0.01064 0.00448 -0.0283 0.0593 0.9216
5.750 0.7549 0.01082 0.00467 -0.0278 0.0566 0.9311
6.000 0.7786 0.01111 0.00496 -0.0269 0.0534 0.9434
6.250 0.8023 0.01123 0.00513 -0.0260 0.0518 0.9587
6.500 0.8288 0.01141 0.00532 -0.0257 0.0496 0.9776
6.750 0.8595 0.01180 0.00568 -0.0265 0.0470 1.0000
7.000 0.8874 0.01201 0.00590 -0.0267 0.0457 1.0000
7.250 0.9147 0.01227 0.00615 -0.0267 0.0441 1.0000
7.500 0.9410 0.01261 0.00646 -0.0266 0.0425 1.0000
7.750 0.9663 0.01304 0.00690 -0.0264 0.0410 1.0000
8.000 0.9928 0.01331 0.00718 -0.0262 0.0399 1.0000
8.250 1.0188 0.01360 0.00747 -0.0261 0.0387 1.0000
8.500 1.0443 0.01395 0.00781 -0.0258 0.0375 1.0000
8.750 1.0673 0.01453 0.00838 -0.0252 0.0360 1.0000
9.000 1.0929 0.01482 0.00870 -0.0249 0.0354 1.0000
9.250 1.1178 0.01517 0.00907 -0.0246 0.0345 1.0000
9.500 1.1423 0.01553 0.00945 -0.0242 0.0335 1.0000
9.750 1.1659 0.01596 0.00987 -0.0237 0.0327 1.0000
10.000 1.1861 0.01671 0.01063 -0.0227 0.0315 1.0000
10.250 1.2104 0.01702 0.01099 -0.0222 0.0309 1.0000
10.500 1.2339 0.01740 0.01140 -0.0217 0.0302 1.0000
10.750 1.2566 0.01782 0.01185 -0.0210 0.0294 1.0000
11.000 1.2786 0.01828 0.01232 -0.0203 0.0288 1.0000
11.250 1.2989 0.01886 0.01290 -0.0194 0.0281 1.0000
11.500 1.3149 0.01976 0.01384 -0.0179 0.0273 1.0000
11.750 1.3356 0.02021 0.01435 -0.0169 0.0269 1.0000
12.000 1.3540 0.02071 0.01491 -0.0157 0.0264 1.0000
12.250 1.3708 0.02128 0.01552 -0.0142 0.0259 1.0000
12.500 1.3872 0.02188 0.01617 -0.0127 0.0254 1.0000
12.750 1.4032 0.02253 0.01686 -0.0113 0.0250 1.0000
13.000 1.4183 0.02326 0.01762 -0.0099 0.0245 1.0000
13.250 1.4304 0.02423 0.01862 -0.0082 0.0241 1.0000
13.500 1.4376 0.02561 0.02007 -0.0062 0.0235 1.0000
13.750 1.4533 0.02635 0.02089 -0.0051 0.0233 1.0000
14.000 1.4673 0.02723 0.02185 -0.0039 0.0230 1.0000
14.250 1.4800 0.02823 0.02293 -0.0027 0.0226 1.0000
14.500 1.4918 0.02933 0.02409 -0.0015 0.0223 1.0000
14.750 1.5027 0.03049 0.02533 -0.0004 0.0220 1.0000
15.000 1.5130 0.03174 0.02664 0.0007 0.0217 1.0000
15.250 1.5224 0.03309 0.02805 0.0018 0.0214 1.0000
15.500 1.5305 0.03457 0.02960 0.0028 0.0212 1.0000
15.750 1.5365 0.03628 0.03137 0.0038 0.0210 1.0000
16.000 1.5394 0.03832 0.03348 0.0048 0.0207 1.0000
16.250 1.5373 0.04089 0.03615 0.0057 0.0205 1.0000
16.500 1.5303 0.04408 0.03946 0.0065 0.0202 1.0000
16.750 1.5328 0.04639 0.04188 0.0069 0.0201 1.0000
17.000 1.5338 0.04894 0.04453 0.0071 0.0200 1.0000
17.250 1.5324 0.05185 0.04756 0.0071 0.0199 1.0000
17.500 1.5298 0.05504 0.05088 0.0067 0.0197 1.0000
17.750 1.5250 0.05866 0.05462 0.0061 0.0196 1.0000
18.000 1.5182 0.06274 0.05882 0.0051 0.0195 1.0000
18.250 1.5091 0.06735 0.06358 0.0036 0.0194 1.0000
18.500 1.4972 0.07258 0.06894 0.0015 0.0193 1.0000
18.750 1.4817 0.07866 0.07517 -0.0012 0.0192 1.0000
19.000 1.4628 0.08566 0.08232 -0.0046 0.0191 1.0000
19.250 1.4380 0.09401 0.09084 -0.0091 0.0191 1.0000
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