S1016 (s1016-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: S1016 (s1016-il) Reynolds number: 1,000,000 Max Cl/Cd: 52.2 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s1016-il-1000000.txt Download as CSV file: xf-s1016-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: S1016
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
------ -------- --------- --------- -------- -------- --------
-19.500 -1.2497 0.06214 0.05732 -0.0657 0.8729 0.0226
-19.250 -1.2571 0.05823 0.05333 -0.0668 0.8712 0.0231
-19.000 -1.2589 0.05512 0.05015 -0.0676 0.8694 0.0236
-18.750 -1.2605 0.05215 0.04709 -0.0682 0.8676 0.0241
-18.500 -1.2586 0.04967 0.04452 -0.0685 0.8659 0.0248
-18.250 -1.2544 0.04751 0.04227 -0.0686 0.8642 0.0254
-18.000 -1.2495 0.04546 0.04013 -0.0686 0.8624 0.0258
-17.750 -1.2517 0.04284 0.03743 -0.0684 0.8607 0.0267
-17.500 -1.2488 0.04078 0.03532 -0.0680 0.8590 0.0276
-17.250 -1.2429 0.03903 0.03353 -0.0676 0.8580 0.0284
-17.000 -1.2343 0.03756 0.03200 -0.0672 0.8568 0.0295
-16.750 -1.2247 0.03621 0.03059 -0.0667 0.8556 0.0302
-16.500 -1.2206 0.03448 0.02881 -0.0658 0.8545 0.0313
-16.250 -1.2131 0.03307 0.02738 -0.0650 0.8534 0.0325
-16.000 -1.2030 0.03189 0.02616 -0.0643 0.8523 0.0338
-15.750 -1.1903 0.03092 0.02513 -0.0636 0.8513 0.0349
-15.500 -1.1813 0.02972 0.02389 -0.0626 0.8502 0.0362
-15.250 -1.1714 0.02862 0.02278 -0.0616 0.8492 0.0378
-15.000 -1.1596 0.02768 0.02180 -0.0606 0.8482 0.0392
-14.750 -1.1453 0.02691 0.02097 -0.0598 0.8472 0.0404
-14.500 -1.1336 0.02601 0.02003 -0.0588 0.8461 0.0421
-14.250 -1.1215 0.02515 0.01917 -0.0577 0.8451 0.0440
-14.000 -1.1069 0.02445 0.01844 -0.0567 0.8440 0.0456
-13.750 -1.0908 0.02387 0.01781 -0.0559 0.8428 0.0470
-13.500 -1.0782 0.02307 0.01700 -0.0547 0.8422 0.0494
-13.250 -1.0633 0.02240 0.01634 -0.0537 0.8417 0.0515
-13.000 -1.0466 0.02184 0.01576 -0.0528 0.8411 0.0535
-12.750 -1.0304 0.02127 0.01516 -0.0519 0.8406 0.0553
-12.500 -1.0158 0.02062 0.01452 -0.0507 0.8399 0.0581
-12.250 -0.9987 0.02010 0.01400 -0.0498 0.8393 0.0607
-12.000 -0.9802 0.01966 0.01353 -0.0490 0.8386 0.0623
-11.750 -0.9649 0.01907 0.01295 -0.0478 0.8379 0.0660
-11.500 -0.9478 0.01858 0.01247 -0.0468 0.8370 0.0690
-11.250 -0.9285 0.01819 0.01206 -0.0460 0.8362 0.0714
-11.000 -0.9115 0.01770 0.01158 -0.0449 0.8354 0.0755
-10.750 -0.8936 0.01726 0.01116 -0.0440 0.8347 0.0793
-10.500 -0.8739 0.01692 0.01079 -0.0432 0.8340 0.0821
-10.250 -0.8568 0.01644 0.01036 -0.0420 0.8333 0.0876
-10.000 -0.8373 0.01609 0.01001 -0.0412 0.8326 0.0918
-9.750 -0.8184 0.01572 0.00964 -0.0402 0.8320 0.0967
-9.500 -0.7998 0.01534 0.00929 -0.0392 0.8313 0.1021
-9.250 -0.7794 0.01505 0.00899 -0.0384 0.8306 0.1062
-9.000 -0.7609 0.01467 0.00865 -0.0373 0.8300 0.1128
-8.750 -0.7405 0.01438 0.00837 -0.0365 0.8294 0.1180
-8.500 -0.7215 0.01405 0.00806 -0.0354 0.8287 0.1246
-8.250 -0.7017 0.01377 0.00780 -0.0345 0.8280 0.1310
-8.000 -0.6820 0.01350 0.00756 -0.0335 0.8270 0.1382
-7.750 -0.6624 0.01327 0.00736 -0.0325 0.8259 0.1456
-7.500 -0.6427 0.01299 0.00711 -0.0315 0.8254 0.1540
-7.250 -0.6223 0.01272 0.00688 -0.0305 0.8250 0.1627
-7.000 -0.6031 0.01240 0.00662 -0.0294 0.8246 0.1732
-6.750 -0.5834 0.01212 0.00639 -0.0284 0.8240 0.1841
-6.250 -0.5448 0.01155 0.00593 -0.0261 0.8225 0.2091
-6.000 -0.5262 0.01125 0.00571 -0.0248 0.8216 0.2234
-5.750 -0.5084 0.01096 0.00549 -0.0233 0.8208 0.2403
-5.500 -0.4913 0.01066 0.00528 -0.0217 0.8198 0.2587
-5.250 -0.4751 0.01036 0.00507 -0.0198 0.8186 0.2782
-5.000 -0.4609 0.01011 0.00491 -0.0175 0.8175 0.2993
-4.750 -0.4499 0.00987 0.00477 -0.0146 0.8162 0.3236
-4.500 -0.4362 0.00965 0.00465 -0.0120 0.8150 0.3497
-4.250 -0.4208 0.00937 0.00451 -0.0099 0.8138 0.3800
-4.000 -0.4049 0.00908 0.00435 -0.0078 0.8126 0.4151
-3.750 -0.3882 0.00878 0.00420 -0.0059 0.8114 0.4535
-3.500 -0.3721 0.00848 0.00408 -0.0038 0.8100 0.4970
-3.250 -0.3555 0.00824 0.00403 -0.0019 0.8084 0.5448
-3.000 -0.3375 0.00784 0.00385 -0.0002 0.8072 0.5966
-2.750 -0.3188 0.00743 0.00371 0.0014 0.8055 0.6533
-2.500 -0.2954 0.00726 0.00374 0.0023 0.8034 0.7009
-2.250 -0.2673 0.00724 0.00377 0.0024 0.8011 0.7246
-2.000 -0.2383 0.00724 0.00377 0.0022 0.7989 0.7375
-1.750 -0.2088 0.00720 0.00370 0.0020 0.7965 0.7455
-1.500 -0.1789 0.00719 0.00366 0.0018 0.7942 0.7523
-1.250 -0.1501 0.00728 0.00369 0.0016 0.7914 0.7581
-1.000 -0.1200 0.00726 0.00370 0.0013 0.7891 0.7622
-0.750 -0.0901 0.00727 0.00373 0.0010 0.7857 0.7664
-0.500 -0.0602 0.00725 0.00370 0.0007 0.7824 0.7706
-0.250 -0.0303 0.00723 0.00364 0.0004 0.7797 0.7742
0.000 0.0000 0.00718 0.00358 0.0000 0.7771 0.7771
0.250 0.0303 0.00724 0.00364 -0.0004 0.7742 0.7797
0.500 0.0602 0.00725 0.00371 -0.0007 0.7706 0.7825
0.750 0.0901 0.00727 0.00373 -0.0010 0.7664 0.7858
1.000 0.1200 0.00726 0.00370 -0.0013 0.7621 0.7891
1.250 0.1501 0.00728 0.00369 -0.0016 0.7580 0.7914
1.500 0.1789 0.00719 0.00366 -0.0018 0.7523 0.7942
1.750 0.2088 0.00720 0.00370 -0.0020 0.7455 0.7965
2.000 0.2383 0.00724 0.00377 -0.0022 0.7375 0.7989
2.250 0.2673 0.00724 0.00377 -0.0024 0.7250 0.8011
2.500 0.2954 0.00726 0.00374 -0.0023 0.7009 0.8034
2.750 0.3188 0.00743 0.00371 -0.0014 0.6532 0.8055
3.000 0.3375 0.00783 0.00385 0.0002 0.5968 0.8072
3.250 0.3558 0.00823 0.00403 0.0019 0.5457 0.8084
3.500 0.3721 0.00848 0.00408 0.0038 0.4968 0.8100
3.750 0.3882 0.00878 0.00420 0.0059 0.4532 0.8114
4.000 0.4045 0.00909 0.00435 0.0079 0.4135 0.8126
4.250 0.4207 0.00938 0.00451 0.0099 0.3792 0.8138
4.500 0.4362 0.00965 0.00465 0.0120 0.3494 0.8150
4.750 0.4494 0.00988 0.00478 0.0147 0.3220 0.8162
5.000 0.4609 0.01011 0.00491 0.0175 0.2991 0.8175
5.250 0.4752 0.01036 0.00507 0.0198 0.2781 0.8186
5.500 0.4915 0.01065 0.00527 0.0216 0.2588 0.8198
5.750 0.5086 0.01095 0.00549 0.0233 0.2405 0.8208
6.000 0.5265 0.01125 0.00571 0.0247 0.2240 0.8216
6.250 0.5450 0.01154 0.00593 0.0260 0.2093 0.8225
6.750 0.5832 0.01213 0.00639 0.0284 0.1832 0.8240
7.000 0.6033 0.01240 0.00662 0.0294 0.1732 0.8246
7.250 0.6225 0.01271 0.00687 0.0305 0.1627 0.8250
7.500 0.6431 0.01298 0.00711 0.0314 0.1543 0.8254
7.750 0.6627 0.01326 0.00735 0.0324 0.1459 0.8260
8.000 0.6823 0.01349 0.00755 0.0334 0.1384 0.8270
8.250 0.7020 0.01376 0.00780 0.0344 0.1313 0.8280
8.500 0.7218 0.01405 0.00806 0.0354 0.1246 0.8287
8.750 0.7409 0.01438 0.00836 0.0364 0.1180 0.8294
9.000 0.7611 0.01467 0.00864 0.0373 0.1125 0.8300
9.250 0.7797 0.01504 0.00898 0.0383 0.1062 0.8307
9.500 0.8002 0.01533 0.00928 0.0391 0.1023 0.8313
9.750 0.8188 0.01571 0.00963 0.0401 0.0968 0.8320
10.000 0.8377 0.01608 0.01000 0.0411 0.0919 0.8326
10.250 0.8572 0.01644 0.01035 0.0420 0.0876 0.8333
10.500 0.8743 0.01691 0.01078 0.0431 0.0820 0.8340
10.750 0.8941 0.01725 0.01114 0.0439 0.0793 0.8347
11.000 0.9119 0.01769 0.01157 0.0449 0.0752 0.8354
11.250 0.9291 0.01818 0.01204 0.0459 0.0713 0.8362
11.500 0.9483 0.01857 0.01245 0.0467 0.0689 0.8370
11.750 0.9652 0.01907 0.01295 0.0478 0.0658 0.8379
12.000 0.9806 0.01966 0.01352 0.0490 0.0624 0.8387
12.250 0.9992 0.02008 0.01398 0.0497 0.0605 0.8393
12.500 1.0163 0.02061 0.01450 0.0507 0.0580 0.8399
12.750 1.0310 0.02126 0.01514 0.0518 0.0552 0.8406
13.000 1.0474 0.02181 0.01573 0.0527 0.0533 0.8412
13.250 1.0639 0.02238 0.01632 0.0536 0.0515 0.8417
13.500 1.0789 0.02304 0.01698 0.0546 0.0495 0.8422
13.750 1.0916 0.02384 0.01777 0.0558 0.0470 0.8429
14.000 1.1074 0.02443 0.01843 0.0567 0.0457 0.8440
14.250 1.1223 0.02511 0.01913 0.0576 0.0439 0.8451
14.500 1.1342 0.02599 0.02001 0.0587 0.0420 0.8461
14.750 1.1459 0.02690 0.02096 0.0598 0.0405 0.8472
15.000 1.1604 0.02765 0.02176 0.0606 0.0391 0.8482
15.250 1.1724 0.02857 0.02272 0.0615 0.0378 0.8492
15.500 1.1825 0.02966 0.02383 0.0625 0.0363 0.8502
15.750 1.1914 0.03087 0.02508 0.0635 0.0349 0.8513
16.000 1.2038 0.03185 0.02612 0.0642 0.0339 0.8524
16.250 1.2143 0.03300 0.02730 0.0650 0.0325 0.8535
16.500 1.2219 0.03440 0.02873 0.0658 0.0314 0.8546
16.750 1.2260 0.03612 0.03049 0.0666 0.0301 0.8557
17.000 1.2368 0.03737 0.03181 0.0671 0.0293 0.8569
17.250 1.2444 0.03893 0.03342 0.0675 0.0284 0.8581
17.500 1.2495 0.04074 0.03529 0.0680 0.0277 0.8591
17.750 1.2537 0.04268 0.03728 0.0683 0.0267 0.8608
18.000 1.2511 0.04535 0.04002 0.0685 0.0259 0.8626
18.250 1.2572 0.04726 0.04202 0.0685 0.0253 0.8643
18.500 1.2610 0.04946 0.04431 0.0684 0.0248 0.8660
18.750 1.2628 0.05195 0.04688 0.0681 0.0242 0.8678
19.000 1.2625 0.05476 0.04977 0.0676 0.0237 0.8696
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