NLR-7301 AIRFOIL (nlr7301-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NLR-7301 AIRFOIL (nlr7301-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.24 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-nlr7301-il-1000000-n5.txt Download as CSV file: xf-nlr7301-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3153 0.07902 0.07458 -0.0489 1.0000 0.0243
-19.500 -1.3242 0.07441 0.06988 -0.0509 1.0000 0.0244
-19.250 -1.3304 0.07023 0.06561 -0.0527 1.0000 0.0246
-19.000 -1.3344 0.06644 0.06175 -0.0542 1.0000 0.0248
-18.750 -1.3360 0.06306 0.05830 -0.0554 1.0000 0.0249
-18.500 -1.3355 0.06000 0.05517 -0.0564 1.0000 0.0251
-18.250 -1.3340 0.05709 0.05221 -0.0573 1.0000 0.0253
-18.000 -1.3314 0.05438 0.04943 -0.0581 1.0000 0.0254
-17.750 -1.3268 0.05197 0.04697 -0.0587 1.0000 0.0256
-17.500 -1.3221 0.04958 0.04452 -0.0593 1.0000 0.0258
-17.250 -1.3153 0.04748 0.04237 -0.0597 1.0000 0.0260
-17.000 -1.3086 0.04539 0.04022 -0.0601 1.0000 0.0262
-16.750 -1.3001 0.04354 0.03832 -0.0604 1.0000 0.0264
-16.500 -1.2917 0.04166 0.03639 -0.0606 1.0000 0.0266
-16.250 -1.2816 0.04001 0.03470 -0.0608 1.0000 0.0268
-16.000 -1.2718 0.03836 0.03300 -0.0609 1.0000 0.0270
-15.750 -1.2606 0.03688 0.03147 -0.0610 1.0000 0.0272
-15.500 -1.2490 0.03544 0.02998 -0.0610 1.0000 0.0274
-15.250 -1.2375 0.03404 0.02854 -0.0610 1.0000 0.0275
-15.000 -1.2270 0.03260 0.02707 -0.0609 1.0000 0.0278
-14.750 -1.2155 0.03123 0.02568 -0.0608 1.0000 0.0281
-14.500 -1.2021 0.03005 0.02447 -0.0606 1.0000 0.0284
-14.250 -1.1883 0.02890 0.02330 -0.0605 1.0000 0.0287
-14.000 -1.1704 0.02782 0.02219 -0.0611 0.9774 0.0291
-13.750 -1.1548 0.02685 0.02118 -0.0609 0.9610 0.0294
-13.500 -1.1416 0.02592 0.02019 -0.0601 0.9473 0.0298
-13.250 -1.1273 0.02505 0.01926 -0.0594 0.9357 0.0301
-13.000 -1.1116 0.02423 0.01839 -0.0588 0.9266 0.0305
-12.750 -1.0952 0.02343 0.01753 -0.0583 0.9179 0.0308
-12.500 -1.0779 0.02268 0.01672 -0.0579 0.9110 0.0311
-12.250 -1.0609 0.02183 0.01585 -0.0576 0.9047 0.0317
-12.000 -1.0431 0.02105 0.01505 -0.0573 0.8983 0.0322
-11.500 -1.0045 0.01967 0.01361 -0.0568 0.8878 0.0332
-11.250 -0.9841 0.01901 0.01292 -0.0567 0.8828 0.0337
-11.000 -0.9630 0.01841 0.01229 -0.0566 0.8776 0.0342
-10.750 -0.9416 0.01784 0.01167 -0.0565 0.8724 0.0347
-10.500 -0.9208 0.01727 0.01107 -0.0563 0.8681 0.0353
-10.250 -0.8982 0.01668 0.01048 -0.0565 0.8643 0.0360
-10.000 -0.8737 0.01613 0.00993 -0.0570 0.8604 0.0367
-9.750 -0.8483 0.01563 0.00940 -0.0575 0.8566 0.0375
-9.500 -0.8221 0.01517 0.00892 -0.0581 0.8530 0.0384
-9.250 -0.7953 0.01474 0.00846 -0.0587 0.8494 0.0393
-9.000 -0.7682 0.01428 0.00800 -0.0594 0.8465 0.0404
-8.750 -0.7407 0.01388 0.00761 -0.0599 0.8440 0.0416
-8.500 -0.7130 0.01354 0.00727 -0.0604 0.8411 0.0427
-8.250 -0.6853 0.01321 0.00694 -0.0608 0.8379 0.0439
-8.000 -0.6575 0.01288 0.00661 -0.0612 0.8346 0.0453
-7.750 -0.6295 0.01259 0.00631 -0.0616 0.8314 0.0469
-7.500 -0.6012 0.01232 0.00604 -0.0619 0.8284 0.0485
-7.250 -0.5728 0.01204 0.00576 -0.0623 0.8255 0.0507
-7.000 -0.5439 0.01178 0.00552 -0.0628 0.8236 0.0529
-6.750 -0.5150 0.01150 0.00527 -0.0632 0.8215 0.0553
-6.500 -0.4858 0.01127 0.00505 -0.0636 0.8191 0.0579
-6.250 -0.4566 0.01102 0.00483 -0.0641 0.8166 0.0608
-6.000 -0.4273 0.01080 0.00463 -0.0645 0.8139 0.0640
-5.750 -0.3980 0.01057 0.00443 -0.0649 0.8111 0.0681
-5.500 -0.3685 0.01037 0.00424 -0.0653 0.8084 0.0721
-5.250 -0.3389 0.01018 0.00406 -0.0657 0.8058 0.0766
-5.000 -0.3092 0.00998 0.00389 -0.0662 0.8032 0.0816
-4.750 -0.2792 0.00978 0.00374 -0.0667 0.8016 0.0876
-4.500 -0.2492 0.00958 0.00359 -0.0671 0.7997 0.0942
-3.750 -0.1586 0.00898 0.00316 -0.0686 0.7924 0.1229
-3.500 -0.1283 0.00876 0.00302 -0.0692 0.7902 0.1371
-3.250 -0.0980 0.00852 0.00287 -0.0698 0.7873 0.1577
-3.000 -0.0679 0.00825 0.00270 -0.0703 0.7817 0.1874
-2.750 -0.0372 0.00787 0.00251 -0.0711 0.7760 0.2296
-2.500 -0.0063 0.00742 0.00229 -0.0720 0.7685 0.2901
-2.250 0.0244 0.00695 0.00204 -0.0729 0.7580 0.3621
-2.000 0.0550 0.00646 0.00179 -0.0738 0.7371 0.4452
-1.750 0.0844 0.00631 0.00169 -0.0741 0.7005 0.4971
-1.500 0.1113 0.00650 0.00168 -0.0737 0.6354 0.5180
-1.250 0.1353 0.00704 0.00182 -0.0730 0.5281 0.5302
-1.000 0.1597 0.00761 0.00200 -0.0724 0.4268 0.5394
-0.750 0.1846 0.00815 0.00218 -0.0720 0.3328 0.5477
-0.500 0.2100 0.00865 0.00236 -0.0716 0.2492 0.5611
-0.250 0.2365 0.00903 0.00255 -0.0714 0.1876 0.5783
0.000 0.2639 0.00931 0.00269 -0.0712 0.1491 0.5885
0.250 0.2922 0.00952 0.00280 -0.0712 0.1285 0.5935
0.500 0.3207 0.00969 0.00290 -0.0712 0.1150 0.5959
0.750 0.3493 0.00985 0.00298 -0.0712 0.1055 0.5981
1.000 0.3780 0.01000 0.00307 -0.0712 0.0984 0.6002
1.250 0.4067 0.01016 0.00317 -0.0712 0.0923 0.6019
1.500 0.4354 0.01029 0.00327 -0.0712 0.0876 0.6039
1.750 0.4640 0.01043 0.00337 -0.0712 0.0834 0.6062
2.000 0.4925 0.01057 0.00349 -0.0712 0.0793 0.6085
2.250 0.5209 0.01072 0.00361 -0.0711 0.0757 0.6109
2.500 0.5492 0.01088 0.00374 -0.0710 0.0716 0.6135
2.750 0.5774 0.01104 0.00388 -0.0710 0.0681 0.6161
3.000 0.6054 0.01123 0.00402 -0.0709 0.0644 0.6185
3.250 0.6335 0.01140 0.00416 -0.0708 0.0612 0.6206
3.500 0.6612 0.01159 0.00431 -0.0706 0.0580 0.6225
3.750 0.6889 0.01178 0.00447 -0.0705 0.0551 0.6243
4.000 0.7164 0.01198 0.00464 -0.0703 0.0527 0.6270
4.250 0.7439 0.01217 0.00483 -0.0701 0.0506 0.6296
4.500 0.7710 0.01239 0.00503 -0.0699 0.0489 0.6323
4.750 0.7982 0.01260 0.00523 -0.0696 0.0477 0.6351
5.000 0.8252 0.01282 0.00544 -0.0694 0.0466 0.6380
5.250 0.8520 0.01305 0.00566 -0.0691 0.0457 0.6407
5.500 0.8785 0.01330 0.00588 -0.0688 0.0449 0.6430
5.750 0.9047 0.01357 0.00613 -0.0684 0.0441 0.6449
6.000 0.9309 0.01381 0.00638 -0.0680 0.0436 0.6476
6.250 0.9571 0.01405 0.00663 -0.0676 0.0431 0.6505
6.500 0.9830 0.01431 0.00690 -0.0672 0.0427 0.6533
6.750 1.0086 0.01457 0.00718 -0.0668 0.0423 0.6561
7.000 1.0339 0.01485 0.00746 -0.0662 0.0419 0.6589
7.250 1.0588 0.01515 0.00776 -0.0657 0.0415 0.6615
7.500 1.0834 0.01545 0.00806 -0.0651 0.0411 0.6640
7.750 1.1077 0.01578 0.00838 -0.0644 0.0407 0.6662
8.000 1.1315 0.01611 0.00872 -0.0637 0.0403 0.6689
8.250 1.1547 0.01648 0.00910 -0.0629 0.0399 0.6722
8.500 1.1769 0.01687 0.00951 -0.0620 0.0396 0.6753
8.750 1.1978 0.01722 0.00989 -0.0608 0.0394 0.6781
9.000 1.2186 0.01757 0.01026 -0.0596 0.0392 0.6809
9.250 1.2399 0.01795 0.01067 -0.0585 0.0391 0.6836
9.500 1.2611 0.01835 0.01109 -0.0575 0.0389 0.6861
9.750 1.2818 0.01878 0.01154 -0.0564 0.0388 0.6883
10.000 1.3022 0.01923 0.01201 -0.0553 0.0386 0.6903
10.250 1.3222 0.01969 0.01251 -0.0542 0.0384 0.6934
10.500 1.3418 0.02018 0.01304 -0.0530 0.0383 0.6963
10.750 1.3609 0.02069 0.01359 -0.0518 0.0381 0.6992
11.000 1.3796 0.02123 0.01417 -0.0506 0.0379 0.7021
11.250 1.3979 0.02180 0.01477 -0.0494 0.0378 0.7050
11.500 1.4157 0.02240 0.01540 -0.0482 0.0376 0.7079
11.750 1.4332 0.02303 0.01606 -0.0470 0.0375 0.7105
12.000 1.4501 0.02370 0.01676 -0.0457 0.0373 0.7125
12.250 1.4667 0.02439 0.01750 -0.0444 0.0372 0.7158
12.500 1.4828 0.02511 0.01828 -0.0432 0.0370 0.7187
12.750 1.4983 0.02589 0.01910 -0.0419 0.0369 0.7216
13.000 1.5134 0.02670 0.01996 -0.0406 0.0368 0.7245
13.250 1.5276 0.02758 0.02088 -0.0393 0.0366 0.7273
13.500 1.5415 0.02851 0.02185 -0.0380 0.0365 0.7300
13.750 1.5545 0.02949 0.02288 -0.0367 0.0364 0.7324
14.000 1.5667 0.03055 0.02398 -0.0354 0.0363 0.7344
14.250 1.5785 0.03166 0.02514 -0.0341 0.0362 0.7374
14.500 1.5890 0.03287 0.02642 -0.0328 0.0361 0.7408
14.750 1.5991 0.03414 0.02775 -0.0316 0.0360 0.7441
15.000 1.6074 0.03557 0.02925 -0.0303 0.0358 0.7474
15.250 1.6150 0.03709 0.03083 -0.0290 0.0357 0.7504
15.500 1.6212 0.03876 0.03256 -0.0278 0.0356 0.7531
15.750 1.6262 0.04056 0.03443 -0.0266 0.0355 0.7554
16.000 1.6304 0.04248 0.03643 -0.0256 0.0354 0.7582
16.250 1.6365 0.04430 0.03833 -0.0247 0.0353 0.7617
16.500 1.6430 0.04612 0.04024 -0.0240 0.0353 0.7652
16.750 1.6484 0.04812 0.04232 -0.0234 0.0352 0.7687
17.000 1.6529 0.05027 0.04455 -0.0229 0.0352 0.7721
17.250 1.6572 0.05251 0.04688 -0.0225 0.0351 0.7752
17.500 1.6597 0.05504 0.04949 -0.0223 0.0351 0.7781
17.750 1.6609 0.05776 0.05232 -0.0223 0.0350 0.7815
18.000 1.6607 0.06075 0.05540 -0.0224 0.0350 0.7848
18.250 1.6598 0.06393 0.05869 -0.0228 0.0349 0.7881
18.500 1.6575 0.06740 0.06226 -0.0234 0.0349 0.7915
18.750 1.6536 0.07116 0.06612 -0.0242 0.0348 0.7946
19.000 1.6480 0.07527 0.07035 -0.0253 0.0348 0.7976
19.250 1.6409 0.07970 0.07490 -0.0268 0.0347 0.8011
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