S1016 (s1016-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: S1016 (s1016-il) Reynolds number: 200,000 Max Cl/Cd: 35.28 at α=4.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s1016-il-200000.txt Download as CSV file: xf-s1016-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.9048 0.10863 0.10436 -0.0514 1.0000 0.0519
-18.750 -0.9707 0.09356 0.08889 -0.0603 1.0000 0.0512
-18.500 -0.9998 0.08555 0.08063 -0.0646 1.0000 0.0516
-18.250 -1.0209 0.07925 0.07411 -0.0678 1.0000 0.0523
-18.000 -1.0395 0.07359 0.06821 -0.0702 1.0000 0.0529
-17.750 -1.0566 0.06850 0.06287 -0.0721 1.0000 0.0536
-17.500 -1.0735 0.06393 0.05803 -0.0735 1.0000 0.0543
-17.250 -1.0672 0.06133 0.05542 -0.0739 1.0000 0.0557
-17.000 -1.0582 0.05952 0.05365 -0.0744 1.0000 0.0572
-16.750 -1.0575 0.05694 0.05097 -0.0749 1.0000 0.0585
-16.500 -1.0597 0.05419 0.04806 -0.0752 1.0000 0.0599
-16.250 -1.0642 0.05145 0.04511 -0.0752 1.0000 0.0614
-16.000 -1.0693 0.04890 0.04231 -0.0748 1.0000 0.0625
-15.750 -1.0532 0.04740 0.04091 -0.0749 1.0000 0.0649
-15.500 -1.0457 0.04593 0.03942 -0.0747 1.0000 0.0668
-15.250 -1.0429 0.04430 0.03768 -0.0739 1.0000 0.0687
-15.000 -1.0442 0.04274 0.03594 -0.0725 1.0000 0.0705
-14.750 -1.0541 0.04168 0.03469 -0.0692 1.0000 0.0717
-14.500 -1.0401 0.04059 0.03370 -0.0683 0.9982 0.0743
-14.250 -1.0258 0.03935 0.03244 -0.0687 0.9925 0.0770
-14.000 -1.0137 0.03797 0.03090 -0.0689 0.9892 0.0799
-13.750 -0.9977 0.03654 0.02931 -0.0693 0.9868 0.0830
-13.500 -0.9771 0.03546 0.02831 -0.0701 0.9849 0.0864
-13.250 -0.9591 0.03435 0.02708 -0.0708 0.9831 0.0901
-13.000 -0.9418 0.03317 0.02570 -0.0713 0.9814 0.0936
-12.750 -0.9187 0.03220 0.02483 -0.0719 0.9798 0.0978
-12.500 -0.9024 0.03137 0.02393 -0.0718 0.9774 0.1020
-12.250 -0.8849 0.03047 0.02285 -0.0718 0.9752 0.1062
-12.000 -0.8612 0.02959 0.02207 -0.0724 0.9735 0.1110
-11.750 -0.8407 0.02881 0.02120 -0.0728 0.9717 0.1163
-11.500 -0.8173 0.02797 0.02034 -0.0733 0.9704 0.1218
-11.250 -0.7956 0.02726 0.01964 -0.0737 0.9692 0.1274
-11.000 -0.7753 0.02665 0.01887 -0.0738 0.9678 0.1333
-10.750 -0.7581 0.02605 0.01839 -0.0730 0.9660 0.1394
-10.500 -0.7440 0.02563 0.01790 -0.0717 0.9640 0.1456
-10.250 -0.7264 0.02508 0.01739 -0.0709 0.9624 0.1523
-10.000 -0.7109 0.02469 0.01697 -0.0699 0.9607 0.1595
-9.750 -0.6920 0.02418 0.01649 -0.0693 0.9591 0.1673
-9.500 -0.6727 0.02374 0.01602 -0.0689 0.9574 0.1764
-9.250 -0.6537 0.02325 0.01559 -0.0684 0.9562 0.1855
-9.000 -0.6351 0.02294 0.01521 -0.0677 0.9551 0.1955
-8.750 -0.6213 0.02257 0.01496 -0.0662 0.9538 0.2054
-8.500 -0.6323 0.02281 0.01514 -0.0596 0.9508 0.2117
-8.250 -0.6427 0.02283 0.01526 -0.0533 0.9476 0.2181
-8.000 -0.6468 0.02285 0.01526 -0.0482 0.9455 0.2269
-7.750 -0.6394 0.02257 0.01507 -0.0453 0.9435 0.2387
-7.500 -0.6311 0.02232 0.01489 -0.0426 0.9419 0.2526
-7.250 -0.6247 0.02213 0.01476 -0.0396 0.9407 0.2676
-7.000 -0.6287 0.02207 0.01475 -0.0344 0.9384 0.2818
-6.750 -0.6648 0.02225 0.01496 -0.0231 0.9353 0.2853
-6.500 -0.6791 0.02218 0.01490 -0.0159 0.9324 0.2979
-6.250 -0.6907 0.02203 0.01484 -0.0091 0.9300 0.3130
-6.000 -0.6925 0.02180 0.01472 -0.0042 0.9274 0.3348
-5.750 -0.6884 0.02151 0.01460 -0.0004 0.9256 0.3646
-5.500 -0.6918 0.02123 0.01449 0.0049 0.9226 0.3945
-5.250 -0.7068 0.02089 0.01428 0.0125 0.9196 0.4219
-5.000 -0.7090 0.02042 0.01406 0.0176 0.9161 0.4636
-4.750 -0.7037 0.01996 0.01393 0.0215 0.9133 0.5209
-4.500 -0.6814 0.01978 0.01428 0.0227 0.9105 0.6019
-4.250 -0.6222 0.02121 0.01615 0.0185 0.9088 0.6746
-4.000 -0.6225 0.02179 0.01678 0.0244 0.9037 0.7001
-3.750 -0.6144 0.02204 0.01697 0.0281 0.8988 0.7267
-3.500 -0.5838 0.02280 0.01766 0.0279 0.8952 0.7442
-3.250 -0.5411 0.02377 0.01852 0.0256 0.8925 0.7589
-3.000 -0.5385 0.02440 0.01916 0.0310 0.8850 0.7656
-2.750 -0.5116 0.02497 0.01966 0.0315 0.8803 0.7769
-2.500 -0.4590 0.02620 0.02085 0.0280 0.8778 0.7816
-2.250 -0.4561 0.02642 0.02103 0.0326 0.8699 0.7931
-2.000 -0.4149 0.02740 0.02199 0.0311 0.8656 0.7969
-1.750 -0.3630 0.02836 0.02292 0.0276 0.8626 0.8019
-1.500 -0.3194 0.02884 0.02335 0.0250 0.8601 0.8104
-1.250 -0.3016 0.02948 0.02399 0.0275 0.8510 0.8143
-1.000 -0.2803 0.02948 0.02394 0.0288 0.8457 0.8260
-0.750 -0.2075 0.03036 0.02481 0.0214 0.8445 0.8272
-0.500 -0.1230 0.03115 0.02558 0.0117 0.8438 0.8283
-0.250 -0.0677 0.03168 0.02613 0.0070 0.8373 0.8308
0.000 0.0005 0.03184 0.02629 -0.0001 0.8334 0.8334
0.250 0.0669 0.03168 0.02613 -0.0069 0.8308 0.8374
0.500 0.1233 0.03115 0.02558 -0.0118 0.8283 0.8438
0.750 0.2073 0.03036 0.02480 -0.0214 0.8272 0.8445
1.000 0.2802 0.02950 0.02396 -0.0288 0.8260 0.8458
1.500 0.3199 0.02881 0.02331 -0.0251 0.8103 0.8601
1.750 0.3634 0.02835 0.02291 -0.0276 0.8019 0.8626
2.000 0.4144 0.02741 0.02200 -0.0310 0.7969 0.8655
2.250 0.4561 0.02641 0.02102 -0.0326 0.7931 0.8699
2.500 0.4589 0.02619 0.02084 -0.0279 0.7816 0.8778
2.750 0.5115 0.02498 0.01967 -0.0315 0.7769 0.8804
3.000 0.5383 0.02441 0.01917 -0.0310 0.7657 0.8851
3.250 0.5412 0.02380 0.01855 -0.0257 0.7590 0.8926
3.500 0.5834 0.02282 0.01767 -0.0279 0.7443 0.8952
3.750 0.6142 0.02204 0.01697 -0.0280 0.7268 0.8988
4.000 0.6222 0.02180 0.01679 -0.0244 0.7004 0.9037
4.250 0.6224 0.02121 0.01614 -0.0186 0.6747 0.9088
4.500 0.6818 0.01977 0.01427 -0.0228 0.6021 0.9105
4.750 0.7038 0.01995 0.01392 -0.0215 0.5215 0.9134
5.000 0.7089 0.02041 0.01405 -0.0176 0.4642 0.9160
5.250 0.7066 0.02089 0.01428 -0.0124 0.4218 0.9196
5.500 0.6915 0.02122 0.01448 -0.0048 0.3947 0.9226
5.750 0.6884 0.02151 0.01459 0.0004 0.3643 0.9256
6.000 0.6924 0.02179 0.01471 0.0042 0.3348 0.9274
6.250 0.6908 0.02202 0.01482 0.0091 0.3130 0.9300
6.500 0.6788 0.02217 0.01489 0.0159 0.2978 0.9324
6.750 0.6647 0.02224 0.01494 0.0231 0.2853 0.9353
7.000 0.6278 0.02205 0.01473 0.0346 0.2821 0.9384
7.250 0.6248 0.02212 0.01475 0.0396 0.2678 0.9407
7.500 0.6312 0.02231 0.01488 0.0426 0.2527 0.9420
7.750 0.6396 0.02255 0.01505 0.0453 0.2390 0.9435
8.000 0.6466 0.02283 0.01524 0.0482 0.2269 0.9456
8.250 0.6422 0.02280 0.01523 0.0534 0.2182 0.9476
8.500 0.6322 0.02279 0.01512 0.0597 0.2120 0.9508
8.750 0.6211 0.02254 0.01493 0.0662 0.2056 0.9539
9.000 0.6354 0.02292 0.01519 0.0676 0.1953 0.9551
9.250 0.6540 0.02323 0.01558 0.0683 0.1853 0.9562
9.500 0.6732 0.02372 0.01601 0.0688 0.1762 0.9575
9.750 0.6926 0.02417 0.01647 0.0692 0.1673 0.9592
10.000 0.7113 0.02467 0.01695 0.0698 0.1593 0.9607
10.250 0.7270 0.02507 0.01738 0.0709 0.1523 0.9624
10.500 0.7442 0.02561 0.01788 0.0717 0.1455 0.9641
10.750 0.7587 0.02603 0.01837 0.0729 0.1394 0.9661
11.000 0.7768 0.02666 0.01886 0.0736 0.1330 0.9679
11.250 0.7966 0.02726 0.01963 0.0736 0.1272 0.9692
11.500 0.8182 0.02796 0.02033 0.0732 0.1216 0.9705
11.750 0.8415 0.02881 0.02120 0.0727 0.1160 0.9718
12.000 0.8623 0.02957 0.02206 0.0722 0.1110 0.9736
12.250 0.8869 0.03048 0.02284 0.0716 0.1059 0.9752
12.500 0.9034 0.03136 0.02392 0.0716 0.1019 0.9775
12.750 0.9200 0.03219 0.02482 0.0717 0.0977 0.9799
13.000 0.9445 0.03320 0.02570 0.0710 0.0934 0.9814
13.250 0.9604 0.03434 0.02708 0.0705 0.0900 0.9832
13.500 0.9786 0.03545 0.02828 0.0698 0.0863 0.9850
13.750 0.9998 0.03653 0.02929 0.0690 0.0828 0.9869
14.000 1.0153 0.03797 0.03090 0.0686 0.0798 0.9894
14.250 1.0279 0.03934 0.03243 0.0684 0.0770 0.9927
14.500 1.0420 0.04058 0.03368 0.0680 0.0742 0.9986
14.750 1.0543 0.04160 0.03461 0.0693 0.0717 1.0000
15.000 1.0454 0.04270 0.03590 0.0723 0.0705 1.0000
15.250 1.0441 0.04426 0.03764 0.0737 0.0687 1.0000
15.500 1.0474 0.04589 0.03938 0.0744 0.0667 1.0000
15.750 1.0549 0.04732 0.04081 0.0747 0.0648 1.0000
16.000 1.0717 0.04889 0.04229 0.0745 0.0625 1.0000
16.250 1.0654 0.05145 0.04511 0.0749 0.0613 1.0000
16.500 1.0618 0.05414 0.04802 0.0749 0.0599 1.0000
16.750 1.0595 0.05690 0.05093 0.0747 0.0585 1.0000
17.000 1.0608 0.05940 0.05352 0.0742 0.0571 1.0000
17.250 1.0692 0.06133 0.05542 0.0737 0.0557 1.0000
17.500 1.0752 0.06393 0.05803 0.0732 0.0542 1.0000
17.750 1.0585 0.06847 0.06284 0.0718 0.0535 1.0000
18.000 1.0413 0.07358 0.06820 0.0700 0.0528 1.0000
18.250 1.0225 0.07927 0.07412 0.0675 0.0521 1.0000
18.500 1.0014 0.08562 0.08071 0.0643 0.0517 1.0000
18.750 0.9717 0.09374 0.08907 0.0599 0.0513 1.0000
19.000 0.9114 0.10782 0.10353 0.0516 0.0518 1.0000
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