AH 93-W-215 (ah93w215-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 93-W-215 (ah93w215-il) Reynolds number: 200,000 Max Cl/Cd: 57.6 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w215-il-200000.txt Download as CSV file: xf-ah93w215-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-215
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
------ -------- --------- --------- -------- -------- --------
-17.250 -0.2161 0.16038 0.15690 -0.0404 1.0000 0.0857
-17.000 -0.8164 0.08110 0.07606 -0.0815 1.0000 0.0671
-16.750 -0.8664 0.07214 0.06679 -0.0861 1.0000 0.0671
-16.500 -0.8437 0.07166 0.06646 -0.0853 1.0000 0.0683
-16.250 -0.8557 0.06758 0.06229 -0.0867 1.0000 0.0689
-16.000 -0.8664 0.06390 0.05851 -0.0878 1.0000 0.0696
-15.750 -0.8792 0.06018 0.05467 -0.0887 1.0000 0.0702
-15.500 -0.8917 0.05668 0.05103 -0.0893 1.0000 0.0709
-15.250 -0.9039 0.05349 0.04770 -0.0894 1.0000 0.0718
-15.000 -0.9171 0.05042 0.04446 -0.0891 1.0000 0.0726
-14.750 -0.9314 0.04758 0.04141 -0.0882 1.0000 0.0734
-14.500 -0.9466 0.04504 0.03866 -0.0868 1.0000 0.0741
-14.250 -0.9474 0.04309 0.03664 -0.0854 1.0000 0.0752
-14.000 -0.9302 0.04211 0.03578 -0.0848 1.0000 0.0766
-13.750 -0.9248 0.04089 0.03458 -0.0835 1.0000 0.0778
-13.250 -0.8907 0.03691 0.03035 -0.0871 0.9454 0.0814
-13.000 -0.8377 0.03461 0.02787 -0.0947 0.9156 0.0844
-12.750 -0.7676 0.03286 0.02600 -0.1051 0.8911 0.0883
-12.500 -0.7031 0.03069 0.02337 -0.1159 0.8650 0.0924
-12.250 -0.6404 0.02959 0.02225 -0.1238 0.8428 0.0965
-12.000 -0.6047 0.02851 0.02087 -0.1278 0.8242 0.1001
-11.750 -0.5733 0.02752 0.01972 -0.1298 0.8105 0.1034
-11.500 -0.5494 0.02695 0.01913 -0.1303 0.7985 0.1065
-11.250 -0.5289 0.02630 0.01831 -0.1304 0.7893 0.1099
-11.000 -0.5133 0.02559 0.01745 -0.1294 0.7805 0.1130
-10.750 -0.4862 0.02497 0.01687 -0.1299 0.7735 0.1167
-10.500 -0.4696 0.02447 0.01631 -0.1289 0.7667 0.1205
-10.250 -0.4585 0.02399 0.01566 -0.1270 0.7598 0.1240
-10.000 -0.4337 0.02334 0.01509 -0.1270 0.7540 0.1285
-9.750 -0.4167 0.02292 0.01461 -0.1259 0.7485 0.1329
-9.500 -0.4062 0.02252 0.01408 -0.1235 0.7430 0.1371
-9.250 -0.3850 0.02190 0.01359 -0.1229 0.7380 0.1425
-9.000 -0.3694 0.02152 0.01314 -0.1213 0.7335 0.1479
-8.750 -0.3509 0.02107 0.01265 -0.1202 0.7293 0.1540
-8.500 -0.3392 0.02068 0.01232 -0.1177 0.7247 0.1596
-8.250 -0.3270 0.02042 0.01197 -0.1153 0.7199 0.1656
-8.000 -0.3116 0.01995 0.01160 -0.1135 0.7156 0.1726
-7.750 -0.2975 0.01975 0.01132 -0.1113 0.7120 0.1804
-7.500 -0.2834 0.01943 0.01106 -0.1092 0.7087 0.1886
-7.250 -0.2726 0.01925 0.01088 -0.1062 0.7048 0.1972
-7.000 -0.2604 0.01888 0.01062 -0.1037 0.7008 0.2067
-6.750 -0.2453 0.01862 0.01035 -0.1016 0.6968 0.2178
-6.500 -0.2303 0.01833 0.01010 -0.0995 0.6933 0.2307
-6.250 -0.2144 0.01805 0.00987 -0.0976 0.6903 0.2449
-6.000 -0.2006 0.01782 0.00973 -0.0953 0.6872 0.2614
-5.750 -0.1888 0.01755 0.00959 -0.0925 0.6837 0.2804
-5.500 -0.1760 0.01728 0.00945 -0.0900 0.6799 0.3039
-5.250 -0.1625 0.01698 0.00929 -0.0875 0.6762 0.3324
-5.000 -0.1473 0.01673 0.00918 -0.0852 0.6731 0.3678
-4.750 -0.1300 0.01659 0.00916 -0.0833 0.6703 0.4057
-4.500 -0.1120 0.01662 0.00928 -0.0815 0.6676 0.4396
-4.250 -0.0964 0.01662 0.00941 -0.0791 0.6640 0.4671
-4.000 -0.0781 0.01667 0.00954 -0.0772 0.6602 0.4911
-3.750 -0.0574 0.01674 0.00964 -0.0757 0.6567 0.5126
-3.500 -0.0347 0.01682 0.00972 -0.0746 0.6536 0.5317
-3.250 -0.0104 0.01693 0.00980 -0.0737 0.6510 0.5492
-3.000 0.0152 0.01712 0.00993 -0.0732 0.6483 0.5657
-2.750 0.0339 0.01729 0.01015 -0.0713 0.6448 0.5795
-2.500 0.0544 0.01742 0.01035 -0.0698 0.6409 0.5920
-2.250 0.0756 0.01755 0.01046 -0.0684 0.6375 0.6055
-2.000 0.1006 0.01766 0.01060 -0.0677 0.6344 0.6172
-1.750 0.1265 0.01773 0.01064 -0.0671 0.6315 0.6290
-1.500 0.1543 0.01786 0.01072 -0.0669 0.6289 0.6408
-1.250 0.1763 0.01807 0.01096 -0.0657 0.6257 0.6509
-1.000 0.1936 0.01827 0.01123 -0.0637 0.6218 0.6617
-0.750 0.2155 0.01840 0.01140 -0.0624 0.6180 0.6716
-0.500 0.2399 0.01849 0.01149 -0.0616 0.6146 0.6825
-0.250 0.2671 0.01854 0.01153 -0.0613 0.6118 0.6927
0.000 0.2949 0.01867 0.01162 -0.0610 0.6094 0.7047
0.250 0.3189 0.01893 0.01192 -0.0601 0.6063 0.7148
0.500 0.3316 0.01917 0.01225 -0.0573 0.6017 0.7259
0.750 0.3531 0.01931 0.01244 -0.0560 0.5978 0.7344
1.000 0.3779 0.01939 0.01253 -0.0553 0.5946 0.7439
1.250 0.4060 0.01936 0.01245 -0.0552 0.5918 0.7528
1.500 0.4377 0.01942 0.01248 -0.0556 0.5894 0.7609
1.750 0.4529 0.01966 0.01275 -0.0534 0.5856 0.7711
2.000 0.4667 0.01994 0.01316 -0.0508 0.5809 0.7786
2.250 0.4870 0.02002 0.01324 -0.0493 0.5771 0.7890
2.500 0.5154 0.01998 0.01321 -0.0492 0.5739 0.7970
2.750 0.5459 0.01995 0.01314 -0.0495 0.5714 0.8064
3.000 0.5789 0.02000 0.01312 -0.0503 0.5690 0.8154
3.250 0.5775 0.02041 0.01372 -0.0450 0.5634 0.8262
3.500 0.5937 0.02051 0.01388 -0.0428 0.5590 0.8365
3.750 0.6189 0.02049 0.01386 -0.0421 0.5557 0.8471
4.000 0.6505 0.02036 0.01369 -0.0426 0.5530 0.8565
4.250 0.6861 0.02028 0.01354 -0.0437 0.5506 0.8667
4.500 0.6825 0.02068 0.01413 -0.0381 0.5450 0.8801
4.750 0.6951 0.02078 0.01430 -0.0353 0.5403 0.8934
5.000 0.7213 0.02064 0.01414 -0.0347 0.5369 0.9065
5.250 0.7639 0.02044 0.01390 -0.0372 0.5341 0.9155
5.500 0.8064 0.02037 0.01376 -0.0399 0.5314 0.9254
5.750 0.8135 0.02089 0.01449 -0.0369 0.5246 0.9412
6.000 0.8565 0.02090 0.01452 -0.0400 0.5201 0.9500
6.250 0.9093 0.02074 0.01430 -0.0447 0.5167 0.9555
6.500 0.9696 0.02059 0.01403 -0.0507 0.5135 0.9582
6.750 0.9936 0.02121 0.01486 -0.0512 0.5062 0.9683
7.000 1.0420 0.02120 0.01485 -0.0554 0.5013 0.9727
7.250 1.0950 0.02097 0.01454 -0.0601 0.4975 0.9770
7.500 1.1322 0.02131 0.01496 -0.0627 0.4917 0.9843
7.750 1.1688 0.02151 0.01522 -0.0651 0.4853 0.9934
8.000 1.2198 0.02128 0.01492 -0.0697 0.4805 0.9987
8.250 1.2263 0.02129 0.01493 -0.0664 0.4761 1.0000
8.500 1.1798 0.02151 0.01522 -0.0537 0.4715 1.0000
8.750 1.1823 0.02152 0.01521 -0.0493 0.4665 1.0000
9.000 1.2182 0.02127 0.01485 -0.0507 0.4619 1.0000
9.250 1.2079 0.02171 0.01534 -0.0443 0.4566 1.0000
9.500 1.2074 0.02204 0.01572 -0.0398 0.4506 1.0000
9.750 1.2365 0.02190 0.01550 -0.0400 0.4455 1.0000
10.000 1.2432 0.02232 0.01595 -0.0368 0.4399 1.0000
10.250 1.2425 0.02287 0.01656 -0.0327 0.4333 1.0000
10.500 1.2715 0.02275 0.01636 -0.0329 0.4276 1.0000
10.750 1.2693 0.02354 0.01722 -0.0290 0.4209 1.0000
11.000 1.2767 0.02409 0.01779 -0.0266 0.4142 1.0000
11.250 1.3102 0.02394 0.01752 -0.0273 0.4083 1.0000
11.500 1.2934 0.02545 0.01920 -0.0225 0.4008 1.0000
11.750 1.3118 0.02578 0.01949 -0.0216 0.3944 1.0000
12.000 1.3169 0.02677 0.02051 -0.0197 0.3873 1.0000
12.250 1.3193 0.02792 0.02171 -0.0177 0.3797 1.0000
12.500 1.3407 0.02822 0.02193 -0.0172 0.3729 1.0000
12.750 1.3299 0.03027 0.02410 -0.0147 0.3646 1.0000
13.000 1.3590 0.03012 0.02381 -0.0147 0.3577 1.0000
13.250 1.3408 0.03285 0.02671 -0.0122 0.3493 1.0000
13.500 1.3593 0.03330 0.02708 -0.0117 0.3420 1.0000
13.750 1.3499 0.03573 0.02962 -0.0100 0.3336 1.0000
14.000 1.3614 0.03670 0.03054 -0.0093 0.3260 1.0000
14.250 1.3568 0.03895 0.03286 -0.0081 0.3177 1.0000
14.500 1.3633 0.04034 0.03422 -0.0073 0.3096 1.0000
14.750 1.3613 0.04252 0.03646 -0.0064 0.3016 1.0000
15.000 1.3640 0.04433 0.03826 -0.0056 0.2934 1.0000
15.250 1.3641 0.04645 0.04041 -0.0049 0.2856 1.0000
15.500 1.3647 0.04857 0.04255 -0.0044 0.2776 1.0000
15.750 1.3665 0.05064 0.04463 -0.0038 0.2699 1.0000
16.000 1.3650 0.05309 0.04711 -0.0034 0.2620 1.0000
16.250 1.3684 0.05508 0.04909 -0.0030 0.2544 1.0000
16.500 1.3641 0.05793 0.05200 -0.0028 0.2464 1.0000
16.750 1.3681 0.05994 0.05397 -0.0025 0.2390 1.0000
17.000 1.3622 0.06310 0.05721 -0.0025 0.2310 1.0000
17.250 1.3671 0.06505 0.05910 -0.0023 0.2239 1.0000
17.500 1.3593 0.06855 0.06270 -0.0024 0.2162 1.0000
17.750 1.3642 0.07053 0.06461 -0.0023 0.2090 1.0000
18.000 1.3546 0.07440 0.06859 -0.0027 0.2014 1.0000
18.250 1.3589 0.07648 0.07058 -0.0027 0.1943 1.0000
18.500 1.3485 0.08056 0.07479 -0.0032 0.1871 1.0000
18.750 1.3536 0.08257 0.07669 -0.0033 0.1803 1.0000
19.000 1.3415 0.08700 0.08127 -0.0041 0.1732 1.0000
19.250 1.3467 0.08904 0.08318 -0.0043 0.1666 1.0000
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