AH 93-W-300 (ah93w300-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-300 (ah93w300-il) Reynolds number: 1,000,000 Max Cl/Cd: 74.83 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w300-il-1000000-n5.txt Download as CSV file: xf-ah93w300-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.9924 0.08913 0.08443 -0.0469 1.0000 0.0910
-18.250 -0.9915 0.08629 0.08158 -0.0476 1.0000 0.0935
-18.000 -0.9905 0.08346 0.07872 -0.0483 1.0000 0.0958
-17.750 -0.9905 0.08057 0.07583 -0.0489 1.0000 0.0985
-17.500 -0.9920 0.07753 0.07278 -0.0495 1.0000 0.1016
-17.250 -0.9901 0.07493 0.07017 -0.0499 1.0000 0.1044
-17.000 -0.9915 0.07202 0.06726 -0.0503 1.0000 0.1080
-16.750 -0.9917 0.06924 0.06447 -0.0507 1.0000 0.1113
-16.500 -0.9919 0.06656 0.06179 -0.0509 1.0000 0.1147
-16.250 -0.9940 0.06369 0.05891 -0.0512 1.0000 0.1183
-16.000 -0.9924 0.06132 0.05653 -0.0512 1.0000 0.1217
-15.750 -0.9943 0.05862 0.05383 -0.0512 1.0000 0.1256
-15.500 -0.9915 0.05615 0.05135 -0.0516 0.9990 0.1293
-15.250 -0.9771 0.05302 0.04823 -0.0551 0.9683 0.1343
-15.000 -0.9559 0.04992 0.04500 -0.0599 0.9217 0.1396
-14.750 -0.9549 0.04759 0.04252 -0.0598 0.8801 0.1447
-14.500 -0.9545 0.04524 0.04005 -0.0596 0.8512 0.1494
-14.000 -0.9505 0.04080 0.03546 -0.0595 0.8114 0.1598
-13.750 -0.9504 0.03847 0.03306 -0.0593 0.7944 0.1652
-13.500 -0.9441 0.03661 0.03116 -0.0593 0.7822 0.1702
-13.250 -0.9438 0.03430 0.02880 -0.0592 0.7682 0.1754
-13.000 -0.9374 0.03254 0.02699 -0.0591 0.7574 0.1807
-12.750 -0.9362 0.03041 0.02483 -0.0588 0.7468 0.1858
-12.500 -0.9301 0.02873 0.02310 -0.0585 0.7352 0.1914
-12.250 -0.9253 0.02691 0.02124 -0.0583 0.7264 0.1963
-12.000 -0.9188 0.02525 0.01957 -0.0580 0.7168 0.2018
-11.750 -0.9092 0.02383 0.01809 -0.0578 0.7061 0.2066
-11.500 -0.9029 0.02218 0.01641 -0.0574 0.6978 0.2120
-11.250 -0.8906 0.02094 0.01515 -0.0573 0.6906 0.2174
-11.000 -0.8806 0.01955 0.01374 -0.0570 0.6816 0.2223
-10.750 -0.8690 0.01836 0.01250 -0.0567 0.6714 0.2279
-10.500 -0.8530 0.01742 0.01154 -0.0565 0.6645 0.2325
-10.250 -0.8425 0.01622 0.01033 -0.0559 0.6569 0.2380
-10.000 -0.8341 0.01534 0.00941 -0.0545 0.6487 0.2429
-9.750 -0.8160 0.01466 0.00869 -0.0544 0.6402 0.2474
-9.500 -0.7945 0.01396 0.00798 -0.0550 0.6338 0.2531
-9.250 -0.7691 0.01356 0.00755 -0.0555 0.6251 0.2589
-9.000 -0.7444 0.01314 0.00712 -0.0558 0.6158 0.2658
-8.750 -0.7170 0.01284 0.00681 -0.0563 0.6093 0.2731
-8.500 -0.6891 0.01253 0.00651 -0.0569 0.6026 0.2791
-8.250 -0.6605 0.01229 0.00626 -0.0575 0.5942 0.2845
-8.000 -0.6312 0.01216 0.00607 -0.0580 0.5847 0.2887
-7.750 -0.6012 0.01195 0.00586 -0.0587 0.5786 0.2932
-7.500 -0.5712 0.01175 0.00566 -0.0595 0.5714 0.2985
-7.250 -0.5410 0.01163 0.00551 -0.0601 0.5626 0.3031
-7.000 -0.5102 0.01152 0.00536 -0.0608 0.5553 0.3071
-6.750 -0.4793 0.01134 0.00520 -0.0616 0.5484 0.3121
-6.500 -0.4483 0.01124 0.00507 -0.0624 0.5408 0.3164
-6.250 -0.4173 0.01118 0.00497 -0.0630 0.5322 0.3202
-6.000 -0.3856 0.01108 0.00486 -0.0639 0.5261 0.3237
-5.750 -0.3541 0.01097 0.00474 -0.0647 0.5185 0.3279
-5.500 -0.3228 0.01091 0.00465 -0.0654 0.5109 0.3320
-5.250 -0.2910 0.01086 0.00457 -0.0662 0.5046 0.3357
-5.000 -0.2591 0.01082 0.00450 -0.0670 0.4980 0.3386
-4.750 -0.2275 0.01075 0.00442 -0.0678 0.4903 0.3427
-4.500 -0.1959 0.01071 0.00435 -0.0685 0.4826 0.3469
-4.250 -0.1637 0.01066 0.00430 -0.0694 0.4775 0.3508
-4.000 -0.1318 0.01064 0.00425 -0.0701 0.4707 0.3539
-3.750 -0.1002 0.01065 0.00422 -0.0708 0.4635 0.3568
-3.500 -0.0682 0.01060 0.00417 -0.0717 0.4575 0.3612
-3.250 -0.0360 0.01056 0.00413 -0.0725 0.4524 0.3652
-3.000 -0.0039 0.01056 0.00411 -0.0732 0.4471 0.3686
-2.750 0.0277 0.01058 0.00410 -0.0739 0.4410 0.3719
-2.500 0.0595 0.01060 0.00409 -0.0746 0.4353 0.3750
-2.250 0.0918 0.01056 0.00407 -0.0755 0.4309 0.3789
-2.000 0.1239 0.01055 0.00406 -0.0762 0.4261 0.3827
-1.750 0.1556 0.01058 0.00407 -0.0769 0.4209 0.3865
-1.500 0.1869 0.01064 0.00409 -0.0775 0.4149 0.3895
-1.250 0.2189 0.01066 0.00410 -0.0782 0.4110 0.3918
-1.000 0.2509 0.01065 0.00410 -0.0790 0.4064 0.3960
-0.750 0.2826 0.01068 0.00412 -0.0797 0.4011 0.3998
-0.500 0.3137 0.01074 0.00416 -0.0802 0.3951 0.4033
-0.250 0.3452 0.01078 0.00419 -0.0808 0.3906 0.4065
0.000 0.3768 0.01083 0.00423 -0.0815 0.3861 0.4094
0.250 0.4078 0.01089 0.00427 -0.0820 0.3805 0.4120
0.500 0.4386 0.01096 0.00433 -0.0825 0.3747 0.4157
0.750 0.4698 0.01101 0.00438 -0.0831 0.3701 0.4192
1.000 0.5011 0.01106 0.00443 -0.0837 0.3654 0.4228
1.250 0.5316 0.01115 0.00450 -0.0841 0.3597 0.4262
1.500 0.5614 0.01128 0.00459 -0.0844 0.3537 0.4289
1.750 0.5921 0.01135 0.00466 -0.0848 0.3493 0.4309
2.000 0.6226 0.01142 0.00473 -0.0853 0.3441 0.4347
2.250 0.6523 0.01154 0.00484 -0.0856 0.3380 0.4385
2.500 0.6818 0.01166 0.00494 -0.0859 0.3327 0.4423
2.750 0.7117 0.01175 0.00504 -0.0862 0.3279 0.4457
3.000 0.7407 0.01189 0.00515 -0.0863 0.3221 0.4484
3.250 0.7687 0.01207 0.00529 -0.0863 0.3160 0.4508
3.500 0.7981 0.01217 0.00540 -0.0865 0.3117 0.4541
3.750 0.8267 0.01230 0.00554 -0.0866 0.3065 0.4582
4.000 0.8539 0.01248 0.00570 -0.0865 0.3006 0.4617
4.250 0.8817 0.01263 0.00585 -0.0865 0.2961 0.4650
4.500 0.9092 0.01278 0.00600 -0.0863 0.2912 0.4683
4.750 0.9350 0.01299 0.00619 -0.0859 0.2855 0.4711
5.000 0.9601 0.01321 0.00638 -0.0854 0.2805 0.4732
5.250 0.9860 0.01337 0.00655 -0.0850 0.2760 0.4764
5.500 1.0100 0.01359 0.00677 -0.0843 0.2705 0.4800
5.750 1.0298 0.01384 0.00701 -0.0829 0.2653 0.4834
6.000 1.0499 0.01403 0.00722 -0.0814 0.2614 0.4869
6.250 1.0702 0.01431 0.00749 -0.0800 0.2564 0.4901
6.500 1.0901 0.01469 0.00785 -0.0787 0.2509 0.4928
6.750 1.1130 0.01499 0.00816 -0.0780 0.2467 0.4950
7.000 1.1345 0.01536 0.00851 -0.0770 0.2415 0.4966
7.250 1.1539 0.01583 0.00896 -0.0758 0.2358 0.5000
7.500 1.1758 0.01620 0.00935 -0.0750 0.2314 0.5041
7.750 1.1955 0.01667 0.00983 -0.0740 0.2258 0.5078
8.000 1.2136 0.01723 0.01038 -0.0728 0.2207 0.5110
8.250 1.2335 0.01774 0.01089 -0.0718 0.2158 0.5139
8.500 1.2508 0.01838 0.01153 -0.0707 0.2106 0.5165
8.750 1.2682 0.01905 0.01219 -0.0696 0.2060 0.5190
9.000 1.2858 0.01973 0.01287 -0.0686 0.2014 0.5211
9.250 1.3013 0.02056 0.01368 -0.0674 0.1965 0.5235
9.500 1.3181 0.02135 0.01451 -0.0665 0.1926 0.5278
9.750 1.3348 0.02218 0.01536 -0.0657 0.1884 0.5314
10.000 1.3482 0.02323 0.01641 -0.0647 0.1839 0.5347
10.250 1.3635 0.02420 0.01740 -0.0639 0.1803 0.5379
10.500 1.3784 0.02523 0.01845 -0.0631 0.1765 0.5413
10.750 1.3899 0.02652 0.01975 -0.0621 0.1724 0.5443
11.000 1.4031 0.02772 0.02096 -0.0613 0.1691 0.5469
11.250 1.4153 0.02903 0.02229 -0.0606 0.1656 0.5488
11.500 1.4263 0.03044 0.02371 -0.0598 0.1620 0.5525
11.750 1.4353 0.03206 0.02537 -0.0591 0.1588 0.5567
12.000 1.4476 0.03345 0.02680 -0.0585 0.1558 0.5606
12.250 1.4552 0.03526 0.02864 -0.0579 0.1525 0.5643
12.500 1.4620 0.03714 0.03054 -0.0572 0.1493 0.5679
12.750 1.4705 0.03897 0.03242 -0.0567 0.1468 0.5716
13.000 1.4790 0.04077 0.03425 -0.0562 0.1439 0.5748
13.250 1.4824 0.04312 0.03663 -0.0557 0.1410 0.5772
13.500 1.4882 0.04524 0.03878 -0.0553 0.1385 0.5810
13.750 1.4935 0.04751 0.04111 -0.0550 0.1362 0.5859
14.000 1.4991 0.04972 0.04337 -0.0548 0.1335 0.5904
14.250 1.4992 0.05255 0.04625 -0.0545 0.1310 0.5944
14.500 1.5027 0.05504 0.04877 -0.0543 0.1287 0.5986
14.750 1.5046 0.05775 0.05155 -0.0542 0.1266 0.6027
15.000 1.5075 0.06032 0.05416 -0.0541 0.1242 0.6061
15.250 1.5043 0.06361 0.05749 -0.0540 0.1220 0.6087
15.500 1.5056 0.06646 0.06039 -0.0541 0.1201 0.6142
15.750 1.5055 0.06951 0.06352 -0.0542 0.1182 0.6195
16.000 1.5067 0.07237 0.06644 -0.0543 0.1160 0.6243
16.250 1.5010 0.07608 0.07020 -0.0546 0.1138 0.6287
16.500 1.4991 0.07933 0.07350 -0.0548 0.1119 0.6333
16.750 1.4967 0.08273 0.07696 -0.0552 0.1099 0.6374
17.250 1.4889 0.08986 0.08420 -0.0561 0.1056 0.6468
17.500 1.4869 0.09324 0.08764 -0.0566 0.1037 0.6527
17.750 1.4833 0.09688 0.09136 -0.0573 0.1020 0.6580
18.000 1.4829 0.10010 0.09463 -0.0579 0.1001 0.6633
18.250 1.4760 0.10413 0.09871 -0.0588 0.0982 0.6676
18.500 1.4728 0.10771 0.10232 -0.0596 0.0965 0.6714
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