NLR-7301 AIRFOIL (nlr7301-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NLR-7301 AIRFOIL (nlr7301-il) Reynolds number: 1,000,000 Max Cl/Cd: 67.12 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-nlr7301-il-1000000.txt Download as CSV file: xf-nlr7301-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NLR-7301 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2614 0.08570 0.08157 -0.0471 1.0000 0.0289
-19.500 -1.2661 0.08152 0.07732 -0.0490 1.0000 0.0290
-19.250 -1.2695 0.07761 0.07334 -0.0507 1.0000 0.0292
-19.000 -1.2717 0.07395 0.06960 -0.0522 1.0000 0.0293
-18.750 -1.2730 0.07043 0.06601 -0.0537 1.0000 0.0295
-18.500 -1.2734 0.06707 0.06258 -0.0550 1.0000 0.0297
-18.250 -1.2727 0.06395 0.05938 -0.0561 1.0000 0.0299
-18.000 -1.2700 0.06112 0.05648 -0.0571 1.0000 0.0301
-17.750 -1.2669 0.05836 0.05364 -0.0580 1.0000 0.0304
-17.500 -1.2626 0.05579 0.05101 -0.0587 1.0000 0.0306
-17.250 -1.2570 0.05343 0.04858 -0.0594 1.0000 0.0308
-17.000 -1.2511 0.05114 0.04622 -0.0600 1.0000 0.0309
-16.750 -1.2432 0.04909 0.04410 -0.0604 1.0000 0.0311
-16.500 -1.2409 0.04658 0.04153 -0.0608 1.0000 0.0313
-16.250 -1.2378 0.04422 0.03913 -0.0610 1.0000 0.0316
-16.000 -1.2324 0.04206 0.03694 -0.0613 1.0000 0.0319
-15.750 -1.2239 0.04026 0.03511 -0.0615 1.0000 0.0322
-15.500 -1.2148 0.03853 0.03334 -0.0616 1.0000 0.0325
-15.250 -1.2039 0.03700 0.03178 -0.0617 1.0000 0.0328
-15.000 -1.1928 0.03552 0.03026 -0.0617 1.0000 0.0331
-14.750 -1.1812 0.03413 0.02884 -0.0617 1.0000 0.0334
-14.500 -1.1687 0.03284 0.02752 -0.0616 1.0000 0.0338
-14.250 -1.1559 0.03157 0.02620 -0.0615 1.0000 0.0341
-14.000 -1.1416 0.03044 0.02503 -0.0614 1.0000 0.0344
-13.750 -1.1265 0.02937 0.02392 -0.0614 1.0000 0.0347
-13.500 -1.1104 0.02836 0.02288 -0.0613 1.0000 0.0350
-13.250 -1.1012 0.02684 0.02134 -0.0611 1.0000 0.0355
-13.000 -1.0877 0.02564 0.02014 -0.0610 1.0000 0.0360
-12.750 -1.0679 0.02465 0.01914 -0.0617 0.9930 0.0365
-12.500 -1.0441 0.02374 0.01822 -0.0629 0.9815 0.0371
-12.250 -1.0254 0.02293 0.01737 -0.0629 0.9685 0.0377
-12.000 -1.0097 0.02222 0.01661 -0.0620 0.9567 0.0382
-11.750 -0.9935 0.02157 0.01590 -0.0611 0.9473 0.0387
-11.500 -0.9760 0.02088 0.01516 -0.0605 0.9389 0.0392
-11.250 -0.9629 0.01989 0.01413 -0.0597 0.9306 0.0399
-11.000 -0.9447 0.01911 0.01334 -0.0594 0.9239 0.0407
-10.750 -0.9253 0.01847 0.01267 -0.0590 0.9173 0.0414
-10.500 -0.9047 0.01788 0.01204 -0.0588 0.9114 0.0421
-10.250 -0.8835 0.01733 0.01146 -0.0587 0.9067 0.0429
-10.000 -0.8610 0.01682 0.01091 -0.0587 0.9019 0.0436
-9.750 -0.8391 0.01606 0.01014 -0.0591 0.8970 0.0448
-9.500 -0.8143 0.01553 0.00959 -0.0596 0.8920 0.0458
-9.250 -0.7876 0.01506 0.00912 -0.0602 0.8890 0.0471
-9.000 -0.7603 0.01467 0.00871 -0.0608 0.8857 0.0481
-8.750 -0.7341 0.01408 0.00813 -0.0616 0.8820 0.0499
-8.500 -0.7071 0.01370 0.00774 -0.0620 0.8784 0.0514
-8.250 -0.6797 0.01340 0.00740 -0.0623 0.8747 0.0529
-8.000 -0.6526 0.01300 0.00701 -0.0627 0.8703 0.0549
-7.750 -0.6245 0.01267 0.00670 -0.0631 0.8681 0.0571
-7.500 -0.5962 0.01236 0.00639 -0.0636 0.8655 0.0594
-7.250 -0.5679 0.01203 0.00609 -0.0640 0.8627 0.0623
-7.000 -0.5393 0.01175 0.00582 -0.0644 0.8599 0.0654
-6.750 -0.5106 0.01146 0.00556 -0.0648 0.8571 0.0690
-6.500 -0.4819 0.01119 0.00530 -0.0652 0.8543 0.0729
-6.250 -0.4528 0.01098 0.00509 -0.0656 0.8510 0.0772
-6.000 -0.4236 0.01073 0.00487 -0.0661 0.8475 0.0825
-5.750 -0.3942 0.01047 0.00466 -0.0666 0.8457 0.0885
-5.500 -0.3646 0.01022 0.00446 -0.0671 0.8436 0.0953
-5.250 -0.3348 0.00998 0.00427 -0.0676 0.8412 0.1032
-5.000 -0.3050 0.00974 0.00408 -0.0681 0.8388 0.1130
-4.750 -0.2752 0.00947 0.00389 -0.0686 0.8363 0.1256
-4.500 -0.2453 0.00919 0.00369 -0.0692 0.8338 0.1422
-4.250 -0.2152 0.00887 0.00349 -0.0698 0.8312 0.1665
-4.000 -0.1849 0.00848 0.00327 -0.0706 0.8284 0.2069
-3.750 -0.1542 0.00798 0.00303 -0.0717 0.8254 0.2684
-3.500 -0.1229 0.00731 0.00272 -0.0731 0.8238 0.3523
-3.250 -0.0910 0.00656 0.00241 -0.0745 0.8215 0.4629
-3.000 -0.0600 0.00631 0.00233 -0.0751 0.8172 0.5126
-2.750 -0.0296 0.00621 0.00228 -0.0754 0.8121 0.5340
-2.500 0.0007 0.00618 0.00223 -0.0756 0.8060 0.5478
-2.250 0.0309 0.00614 0.00219 -0.0757 0.7988 0.5586
-2.000 0.0605 0.00606 0.00208 -0.0757 0.7867 0.5666
-1.750 0.0902 0.00603 0.00203 -0.0757 0.7734 0.5741
-1.500 0.1201 0.00605 0.00198 -0.0757 0.7625 0.5799
-1.250 0.1504 0.00603 0.00197 -0.0759 0.7540 0.5852
-1.000 0.1804 0.00603 0.00197 -0.0761 0.7436 0.5907
-0.750 0.2103 0.00607 0.00197 -0.0762 0.7301 0.5965
-0.500 0.2397 0.00616 0.00200 -0.0761 0.7092 0.6050
-0.250 0.2674 0.00633 0.00208 -0.0757 0.6697 0.6151
0.000 0.2895 0.00703 0.00227 -0.0745 0.5506 0.6208
0.250 0.3104 0.00793 0.00258 -0.0733 0.4125 0.6232
0.500 0.3330 0.00862 0.00281 -0.0725 0.3021 0.6260
0.750 0.3573 0.00916 0.00301 -0.0720 0.2218 0.6288
1.000 0.3832 0.00957 0.00319 -0.0716 0.1707 0.6310
1.250 0.4102 0.00987 0.00334 -0.0714 0.1410 0.6334
1.500 0.4378 0.01012 0.00349 -0.0712 0.1231 0.6357
1.750 0.4657 0.01033 0.00362 -0.0711 0.1117 0.6379
2.000 0.4939 0.01051 0.00375 -0.0710 0.1039 0.6400
2.250 0.5222 0.01069 0.00388 -0.0710 0.0975 0.6420
2.500 0.5502 0.01089 0.00402 -0.0709 0.0918 0.6437
2.750 0.5783 0.01108 0.00415 -0.0708 0.0869 0.6452
3.000 0.6063 0.01122 0.00428 -0.0707 0.0824 0.6489
3.250 0.6338 0.01141 0.00444 -0.0705 0.0777 0.6517
3.500 0.6617 0.01158 0.00460 -0.0704 0.0735 0.6542
3.750 0.6891 0.01180 0.00478 -0.0702 0.0691 0.6566
4.000 0.7162 0.01204 0.00498 -0.0699 0.0650 0.6590
4.250 0.7436 0.01225 0.00517 -0.0697 0.0618 0.6614
4.500 0.7702 0.01253 0.00540 -0.0694 0.0589 0.6637
4.750 0.7974 0.01276 0.00561 -0.0691 0.0571 0.6657
5.000 0.8241 0.01301 0.00583 -0.0688 0.0555 0.6674
5.250 0.8502 0.01326 0.00608 -0.0684 0.0540 0.6715
5.500 0.8763 0.01353 0.00637 -0.0680 0.0530 0.6746
5.750 0.9026 0.01378 0.00663 -0.0676 0.0521 0.6774
6.000 0.9286 0.01405 0.00690 -0.0672 0.0513 0.6801
6.250 0.9543 0.01433 0.00718 -0.0668 0.0506 0.6827
6.500 0.9795 0.01465 0.00749 -0.0662 0.0499 0.6853
6.750 1.0039 0.01502 0.00784 -0.0656 0.0492 0.6876
7.000 1.0271 0.01548 0.00829 -0.0648 0.0484 0.6894
7.250 1.0521 0.01574 0.00858 -0.0642 0.0481 0.6929
7.500 1.0763 0.01605 0.00892 -0.0636 0.0477 0.6962
7.750 1.1001 0.01639 0.00929 -0.0628 0.0474 0.6991
8.000 1.1233 0.01675 0.00968 -0.0620 0.0470 0.7020
8.250 1.1458 0.01713 0.01007 -0.0611 0.0467 0.7049
8.500 1.1664 0.01751 0.01047 -0.0598 0.0463 0.7078
8.750 1.1863 0.01791 0.01089 -0.0585 0.0460 0.7103
9.000 1.2068 0.01836 0.01134 -0.0573 0.0457 0.7121
9.250 1.2274 0.01881 0.01181 -0.0562 0.0454 0.7158
9.500 1.2470 0.01931 0.01235 -0.0550 0.0451 0.7191
9.750 1.2658 0.01987 0.01294 -0.0537 0.0448 0.7220
10.000 1.2832 0.02052 0.01361 -0.0522 0.0445 0.7249
10.250 1.2992 0.02129 0.01440 -0.0506 0.0442 0.7277
10.500 1.3137 0.02219 0.01534 -0.0489 0.0439 0.7304
10.750 1.3308 0.02289 0.01607 -0.0475 0.0437 0.7328
11.000 1.3484 0.02353 0.01674 -0.0463 0.0436 0.7346
11.250 1.3660 0.02417 0.01745 -0.0451 0.0435 0.7385
11.500 1.3826 0.02487 0.01821 -0.0438 0.0434 0.7418
11.750 1.3988 0.02562 0.01901 -0.0425 0.0433 0.7450
12.000 1.4146 0.02641 0.01985 -0.0412 0.0431 0.7480
12.250 1.4295 0.02726 0.02075 -0.0398 0.0430 0.7510
12.500 1.4444 0.02813 0.02166 -0.0385 0.0429 0.7537
12.750 1.4584 0.02907 0.02265 -0.0372 0.0427 0.7558
13.000 1.4722 0.03002 0.02366 -0.0359 0.0426 0.7593
13.250 1.4856 0.03099 0.02471 -0.0346 0.0424 0.7626
13.500 1.4982 0.03204 0.02582 -0.0333 0.0422 0.7657
13.750 1.5107 0.03312 0.02696 -0.0320 0.0420 0.7687
14.000 1.5219 0.03430 0.02819 -0.0308 0.0419 0.7717
14.250 1.5326 0.03554 0.02949 -0.0295 0.0417 0.7744
14.500 1.5428 0.03686 0.03086 -0.0283 0.0416 0.7768
14.750 1.5522 0.03823 0.03232 -0.0271 0.0415 0.7808
15.000 1.5609 0.03967 0.03383 -0.0260 0.0414 0.7843
15.250 1.5685 0.04124 0.03547 -0.0249 0.0413 0.7878
15.500 1.5760 0.04285 0.03715 -0.0238 0.0412 0.7911
15.750 1.5822 0.04459 0.03896 -0.0228 0.0410 0.7941
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