AH 93-W-300 (ah93w300-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 93-W-300 (ah93w300-il) Reynolds number: 1,000,000 Max Cl/Cd: 80.4 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w300-il-1000000.txt Download as CSV file: xf-ah93w300-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-300
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
------ -------- --------- --------- -------- -------- --------
-19.250 -1.0525 0.09130 0.08690 -0.0458 1.0000 0.1089
-19.000 -1.0493 0.08872 0.08429 -0.0465 1.0000 0.1120
-18.750 -1.0581 0.08482 0.08039 -0.0474 1.0000 0.1157
-18.500 -1.0567 0.08210 0.07767 -0.0480 1.0000 0.1194
-18.250 -1.0629 0.07856 0.07411 -0.0487 1.0000 0.1232
-18.000 -1.0637 0.07568 0.07123 -0.0493 1.0000 0.1273
-17.750 -1.0654 0.07273 0.06828 -0.0497 1.0000 0.1312
-17.500 -1.0705 0.06948 0.06503 -0.0502 1.0000 0.1357
-17.250 -1.0694 0.06691 0.06245 -0.0505 1.0000 0.1399
-17.000 -1.0772 0.06348 0.05902 -0.0508 1.0000 0.1449
-16.750 -1.0755 0.06109 0.05664 -0.0510 1.0000 0.1495
-16.500 -1.0842 0.05770 0.05325 -0.0511 1.0000 0.1547
-16.250 -1.0814 0.05552 0.05107 -0.0510 1.0000 0.1595
-16.000 -1.0912 0.05223 0.04778 -0.0508 1.0000 0.1649
-15.750 -1.0887 0.05016 0.04572 -0.0506 1.0000 0.1698
-15.500 -1.0974 0.04716 0.04272 -0.0501 1.0000 0.1749
-15.250 -1.0967 0.04510 0.04067 -0.0495 1.0000 0.1800
-15.000 -1.1009 0.04270 0.03828 -0.0487 1.0000 0.1847
-14.750 -1.1054 0.04039 0.03597 -0.0477 1.0000 0.1898
-14.500 -1.1041 0.03868 0.03426 -0.0467 1.0000 0.1942
-14.250 -1.0993 0.03579 0.03138 -0.0483 0.9969 0.2001
-14.000 -1.0781 0.03395 0.02954 -0.0506 0.9808 0.2057
-13.750 -1.0557 0.03105 0.02664 -0.0555 0.9640 0.2126
-13.500 -1.0237 0.02944 0.02496 -0.0596 0.9360 0.2185
-13.250 -1.0219 0.02729 0.02269 -0.0595 0.8988 0.2238
-13.000 -1.0142 0.02588 0.02118 -0.0589 0.8726 0.2287
-12.750 -1.0044 0.02456 0.01976 -0.0585 0.8516 0.2329
-12.500 -0.9999 0.02290 0.01803 -0.0579 0.8325 0.2382
-12.250 -0.9898 0.02153 0.01661 -0.0577 0.8183 0.2432
-12.000 -0.9763 0.02048 0.01549 -0.0574 0.8034 0.2476
-11.750 -0.9678 0.01903 0.01400 -0.0570 0.7906 0.2528
-11.500 -0.9530 0.01802 0.01294 -0.0569 0.7792 0.2576
-11.250 -0.9371 0.01716 0.01201 -0.0566 0.7663 0.2619
-11.000 -0.9253 0.01599 0.01083 -0.0562 0.7575 0.2670
-10.750 -0.9102 0.01518 0.00998 -0.0557 0.7475 0.2717
-10.500 -0.8963 0.01463 0.00934 -0.0546 0.7356 0.2752
-10.250 -0.8789 0.01379 0.00849 -0.0547 0.7273 0.2806
-10.000 -0.8547 0.01329 0.00798 -0.0553 0.7194 0.2856
-9.750 -0.8279 0.01304 0.00767 -0.0557 0.7101 0.2895
-9.500 -0.8026 0.01269 0.00728 -0.0560 0.6996 0.2944
-9.250 -0.7751 0.01237 0.00697 -0.0565 0.6932 0.2995
-9.000 -0.7461 0.01219 0.00676 -0.0570 0.6848 0.3044
-8.750 -0.7182 0.01196 0.00649 -0.0575 0.6753 0.3100
-8.500 -0.6891 0.01173 0.00627 -0.0581 0.6676 0.3153
-8.250 -0.6587 0.01159 0.00610 -0.0588 0.6606 0.3196
-8.000 -0.6285 0.01148 0.00594 -0.0594 0.6517 0.3230
-7.750 -0.5993 0.01129 0.00573 -0.0600 0.6412 0.3281
-7.500 -0.5682 0.01113 0.00558 -0.0608 0.6357 0.3326
-7.250 -0.5369 0.01104 0.00546 -0.0615 0.6278 0.3365
-7.000 -0.5062 0.01098 0.00533 -0.0622 0.6183 0.3400
-6.750 -0.4754 0.01082 0.00518 -0.0629 0.6102 0.3449
-6.500 -0.4437 0.01071 0.00506 -0.0638 0.6037 0.3490
-6.250 -0.4123 0.01066 0.00497 -0.0645 0.5953 0.3527
-6.000 -0.3812 0.01067 0.00490 -0.0651 0.5849 0.3554
-5.750 -0.3492 0.01052 0.00477 -0.0660 0.5794 0.3599
-5.500 -0.3173 0.01042 0.00468 -0.0668 0.5720 0.3640
-5.250 -0.2859 0.01040 0.00461 -0.0675 0.5631 0.3678
-5.000 -0.2540 0.01039 0.00456 -0.0683 0.5556 0.3711
-4.750 -0.2218 0.01037 0.00451 -0.0691 0.5487 0.3734
-4.500 -0.1901 0.01029 0.00442 -0.0699 0.5405 0.3783
-4.250 -0.1586 0.01027 0.00437 -0.0706 0.5316 0.3822
-4.000 -0.1261 0.01022 0.00433 -0.0714 0.5257 0.3858
-3.750 -0.0942 0.01023 0.00430 -0.0722 0.5181 0.3889
-3.500 -0.0628 0.01029 0.00428 -0.0728 0.5091 0.3914
-3.250 -0.0305 0.01022 0.00423 -0.0736 0.5035 0.3957
-3.000 0.0018 0.01018 0.00420 -0.0745 0.4974 0.3996
-2.750 0.0335 0.01020 0.00419 -0.0752 0.4902 0.4033
-2.500 0.0649 0.01026 0.00420 -0.0758 0.4823 0.4066
-2.250 0.0974 0.01026 0.00419 -0.0766 0.4777 0.4093
-2.000 0.1294 0.01029 0.00419 -0.0773 0.4720 0.4116
-1.750 0.1610 0.01028 0.00418 -0.0780 0.4655 0.4165
-1.500 0.1924 0.01032 0.00420 -0.0786 0.4586 0.4203
-1.250 0.2248 0.01032 0.00421 -0.0794 0.4545 0.4237
-1.000 0.2567 0.01035 0.00423 -0.0801 0.4492 0.4268
-0.750 0.2879 0.01043 0.00427 -0.0806 0.4432 0.4294
-0.500 0.3186 0.01054 0.00431 -0.0811 0.4361 0.4318
-0.250 0.3511 0.01049 0.00431 -0.0819 0.4325 0.4365
0.000 0.3829 0.01051 0.00435 -0.0826 0.4276 0.4403
0.250 0.4140 0.01058 0.00440 -0.0832 0.4219 0.4438
0.500 0.4442 0.01071 0.00448 -0.0835 0.4151 0.4468
0.750 0.4760 0.01075 0.00452 -0.0842 0.4113 0.4493
1.000 0.5074 0.01081 0.00457 -0.0847 0.4068 0.4514
1.250 0.5382 0.01086 0.00462 -0.0852 0.4014 0.4558
1.500 0.5682 0.01096 0.00471 -0.0856 0.3950 0.4599
1.750 0.5992 0.01102 0.00478 -0.0861 0.3907 0.4633
2.000 0.6303 0.01108 0.00485 -0.0866 0.3862 0.4664
2.250 0.6604 0.01119 0.00494 -0.0870 0.3808 0.4693
2.500 0.6893 0.01136 0.00505 -0.0871 0.3746 0.4718
2.750 0.7195 0.01146 0.00514 -0.0874 0.3701 0.4736
3.000 0.7501 0.01149 0.00521 -0.0879 0.3655 0.4785
3.250 0.7795 0.01160 0.00532 -0.0881 0.3601 0.4825
3.500 0.8073 0.01178 0.00547 -0.0881 0.3537 0.4860
3.750 0.8371 0.01187 0.00558 -0.0883 0.3498 0.4893
4.000 0.8661 0.01200 0.00570 -0.0885 0.3449 0.4922
4.250 0.8937 0.01217 0.00584 -0.0884 0.3394 0.4946
4.500 0.9201 0.01239 0.00602 -0.0880 0.3335 0.4964
4.750 0.9491 0.01247 0.00613 -0.0882 0.3294 0.5004
5.000 0.9764 0.01260 0.00628 -0.0881 0.3243 0.5051
5.250 1.0013 0.01282 0.00648 -0.0875 0.3185 0.5086
5.500 1.0272 0.01300 0.00666 -0.0871 0.3138 0.5118
5.750 1.0530 0.01316 0.00684 -0.0867 0.3091 0.5148
6.000 1.0760 0.01340 0.00705 -0.0858 0.3037 0.5176
6.250 1.0924 0.01369 0.00731 -0.0836 0.2982 0.5199
6.500 1.1144 0.01387 0.00750 -0.0825 0.2942 0.5216
6.750 1.1361 0.01413 0.00776 -0.0814 0.2892 0.5249
7.000 1.1562 0.01450 0.00813 -0.0802 0.2833 0.5296
7.250 1.1797 0.01478 0.00844 -0.0795 0.2789 0.5336
7.500 1.2019 0.01512 0.00879 -0.0787 0.2738 0.5372
7.750 1.2210 0.01559 0.00924 -0.0774 0.2682 0.5406
8.000 1.2418 0.01600 0.00965 -0.0765 0.2635 0.5435
8.250 1.2628 0.01641 0.01007 -0.0755 0.2585 0.5459
8.500 1.2802 0.01700 0.01062 -0.0742 0.2532 0.5478
8.750 1.2992 0.01754 0.01116 -0.0732 0.2484 0.5495
9.000 1.3195 0.01803 0.01169 -0.0724 0.2437 0.5555
9.250 1.3362 0.01873 0.01239 -0.0713 0.2383 0.5603
9.500 1.3534 0.01942 0.01311 -0.0702 0.2336 0.5642
9.750 1.3718 0.02009 0.01379 -0.0694 0.2289 0.5678
10.000 1.3859 0.02102 0.01471 -0.0682 0.2236 0.5710
10.250 1.4020 0.02187 0.01557 -0.0672 0.2192 0.5738
10.500 1.4179 0.02275 0.01645 -0.0663 0.2146 0.5762
10.750 1.4292 0.02395 0.01763 -0.0651 0.2096 0.5780
11.000 1.4446 0.02494 0.01867 -0.0644 0.2055 0.5845
11.250 1.4585 0.02608 0.01984 -0.0637 0.2012 0.5900
11.500 1.4687 0.02747 0.02125 -0.0627 0.1966 0.5944
11.750 1.4803 0.02881 0.02261 -0.0619 0.1929 0.5985
12.000 1.4931 0.03006 0.02389 -0.0612 0.1890 0.6023
12.250 1.4996 0.03185 0.02569 -0.0602 0.1850 0.6054
12.500 1.5087 0.03345 0.02730 -0.0594 0.1815 0.6078
12.750 1.5188 0.03507 0.02896 -0.0589 0.1782 0.6130
13.000 1.5269 0.03683 0.03077 -0.0583 0.1746 0.6200
13.250 1.5283 0.03925 0.03322 -0.0576 0.1709 0.6253
13.500 1.5398 0.04079 0.03481 -0.0572 0.1683 0.6305
13.750 1.5450 0.04297 0.03704 -0.0567 0.1652 0.6349
14.000 1.5481 0.04530 0.03938 -0.0562 0.1619 0.6383
14.250 1.5486 0.04796 0.04208 -0.0557 0.1590 0.6411
14.500 1.5571 0.04990 0.04409 -0.0555 0.1564 0.6496
14.750 1.5584 0.05261 0.04686 -0.0553 0.1536 0.6563
15.000 1.5584 0.05542 0.04971 -0.0550 0.1507 0.6622
15.250 1.5570 0.05841 0.05276 -0.0548 0.1483 0.6673
15.500 1.5626 0.06069 0.05508 -0.0547 0.1460 0.6715
15.750 1.5607 0.06384 0.05829 -0.0547 0.1434 0.6779
16.000 1.5579 0.06709 0.06159 -0.0547 0.1407 0.6853
16.250 1.5543 0.07048 0.06505 -0.0548 0.1383 0.6920
16.500 1.5577 0.07305 0.06769 -0.0549 0.1361 0.6987
16.750 1.5532 0.07659 0.07127 -0.0551 0.1336 0.7034
17.000 1.5483 0.08020 0.07494 -0.0554 0.1310 0.7125
17.250 1.5432 0.08388 0.07870 -0.0558 0.1288 0.7204
17.500 1.5458 0.08662 0.08150 -0.0561 0.1267 0.7282
17.750 1.5398 0.09042 0.08536 -0.0567 0.1244 0.7344
18.000 1.5352 0.09409 0.08909 -0.0573 0.1220 0.7439
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