AH 94-W-301 (ah94w301-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 94-W-301 (ah94w301-il) Reynolds number: 500,000 Max Cl/Cd: 77.48 at α=10.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah94w301-il-500000.txt Download as CSV file: xf-ah94w301-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: AH 94-W-301
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.1646 0.09521 0.09050 -0.0314 1.0000 0.1762
-19.000 -1.1726 0.09126 0.08646 -0.0325 1.0000 0.1797
-18.750 -1.1672 0.08907 0.08428 -0.0332 1.0000 0.1830
-18.500 -1.1623 0.08684 0.08209 -0.0339 1.0000 0.1865
-18.250 -1.1652 0.08362 0.07885 -0.0347 1.0000 0.1902
-18.000 -1.1705 0.08015 0.07528 -0.0355 1.0000 0.1937
-17.750 -1.1634 0.07824 0.07342 -0.0360 1.0000 0.1974
-17.500 -1.1624 0.07561 0.07082 -0.0366 1.0000 0.2012
-17.250 -1.1629 0.07278 0.06795 -0.0372 1.0000 0.2050
-17.000 -1.1702 0.06920 0.06426 -0.0379 1.0000 0.2084
-16.750 -1.1600 0.06775 0.06289 -0.0382 1.0000 0.2122
-16.500 -1.1564 0.06550 0.06067 -0.0386 1.0000 0.2160
-16.250 -1.1595 0.06251 0.05762 -0.0390 1.0000 0.2200
-16.000 -1.1602 0.05981 0.05486 -0.0394 1.0000 0.2235
-15.750 -1.1526 0.05817 0.05329 -0.0395 1.0000 0.2275
-15.500 -1.1517 0.05576 0.05088 -0.0397 1.0000 0.2314
-15.250 -1.1514 0.05328 0.04836 -0.0399 1.0000 0.2353
-15.000 -1.1513 0.05086 0.04588 -0.0400 1.0000 0.2388
-14.750 -1.1452 0.04918 0.04428 -0.0399 1.0000 0.2429
-14.500 -1.1421 0.04716 0.04227 -0.0399 1.0000 0.2468
-14.250 -1.1435 0.04470 0.03976 -0.0398 1.0000 0.2508
-14.000 -1.1407 0.04276 0.03779 -0.0396 1.0000 0.2544
-13.750 -1.1366 0.04107 0.03617 -0.0392 1.0000 0.2584
-13.500 -1.1336 0.03926 0.03438 -0.0388 1.0000 0.2623
-13.250 -1.1073 0.03647 0.03149 -0.0441 0.9485 0.2670
-13.000 -1.0440 0.03438 0.02917 -0.0554 0.8708 0.2724
-12.750 -1.0359 0.03307 0.02765 -0.0552 0.8235 0.2764
-12.500 -1.0309 0.03148 0.02591 -0.0550 0.7974 0.2803
-12.250 -1.0272 0.02972 0.02397 -0.0549 0.7779 0.2839
-12.000 -1.0150 0.02874 0.02294 -0.0547 0.7615 0.2877
-11.750 -1.0050 0.02756 0.02171 -0.0545 0.7463 0.2915
-11.500 -0.9953 0.02627 0.02035 -0.0545 0.7332 0.2954
-11.250 -0.9864 0.02492 0.01886 -0.0544 0.7206 0.2990
-11.000 -0.9745 0.02379 0.01767 -0.0544 0.7101 0.3024
-10.750 -0.9606 0.02292 0.01679 -0.0542 0.6997 0.3063
-10.500 -0.9474 0.02193 0.01576 -0.0541 0.6907 0.3100
-10.250 -0.9344 0.02092 0.01468 -0.0540 0.6820 0.3136
-10.000 -0.9230 0.01992 0.01354 -0.0538 0.6734 0.3168
-9.750 -0.9103 0.01922 0.01283 -0.0529 0.6660 0.3204
-9.500 -0.8973 0.01854 0.01215 -0.0523 0.6583 0.3239
-9.250 -0.8778 0.01794 0.01149 -0.0528 0.6508 0.3274
-9.000 -0.8550 0.01743 0.01088 -0.0537 0.6442 0.3311
-8.750 -0.8302 0.01700 0.01037 -0.0546 0.6381 0.3341
-8.500 -0.8046 0.01667 0.01003 -0.0551 0.6318 0.3378
-8.250 -0.7782 0.01642 0.00976 -0.0557 0.6256 0.3413
-8.000 -0.7505 0.01620 0.00951 -0.0566 0.6202 0.3447
-7.750 -0.7220 0.01596 0.00924 -0.0575 0.6147 0.3480
-7.500 -0.6932 0.01577 0.00895 -0.0584 0.6091 0.3510
-7.250 -0.6647 0.01556 0.00870 -0.0592 0.6037 0.3545
-7.000 -0.6355 0.01541 0.00855 -0.0600 0.5986 0.3579
-6.750 -0.6054 0.01525 0.00840 -0.0610 0.5945 0.3611
-6.500 -0.5750 0.01512 0.00824 -0.0620 0.5899 0.3644
-6.250 -0.5445 0.01501 0.00805 -0.0630 0.5852 0.3676
-6.000 -0.5140 0.01492 0.00786 -0.0640 0.5803 0.3702
-5.750 -0.4840 0.01476 0.00774 -0.0648 0.5757 0.3739
-5.500 -0.4530 0.01464 0.00765 -0.0658 0.5722 0.3771
-5.250 -0.4217 0.01456 0.00756 -0.0668 0.5683 0.3803
-5.000 -0.3903 0.01448 0.00744 -0.0678 0.5644 0.3834
-4.750 -0.3588 0.01443 0.00731 -0.0689 0.5603 0.3862
-4.500 -0.3277 0.01439 0.00719 -0.0699 0.5556 0.3892
-4.250 -0.2966 0.01426 0.00713 -0.0708 0.5523 0.3926
-4.000 -0.2650 0.01419 0.00708 -0.0718 0.5490 0.3956
-3.750 -0.2333 0.01413 0.00702 -0.0728 0.5455 0.3985
-3.500 -0.2014 0.01409 0.00695 -0.0738 0.5421 0.4017
-3.250 -0.1694 0.01409 0.00687 -0.0749 0.5386 0.4046
-3.000 -0.1377 0.01408 0.00679 -0.0759 0.5348 0.4074
-2.750 -0.1064 0.01401 0.00677 -0.0767 0.5314 0.4107
-2.500 -0.0747 0.01395 0.00675 -0.0777 0.5285 0.4135
-2.250 -0.0428 0.01393 0.00674 -0.0786 0.5252 0.4166
-2.000 -0.0107 0.01392 0.00671 -0.0796 0.5220 0.4198
-1.750 0.0214 0.01392 0.00667 -0.0806 0.5189 0.4227
-1.500 0.0536 0.01396 0.00664 -0.0816 0.5158 0.4249
-1.250 0.0847 0.01394 0.00663 -0.0825 0.5121 0.4286
-1.000 0.1165 0.01394 0.00667 -0.0833 0.5096 0.4316
-0.750 0.1483 0.01393 0.00670 -0.0842 0.5070 0.4346
-0.500 0.1802 0.01393 0.00671 -0.0851 0.5040 0.4375
-0.250 0.2121 0.01393 0.00670 -0.0860 0.5008 0.4404
0.000 0.2442 0.01397 0.00669 -0.0869 0.4979 0.4431
0.250 0.2757 0.01395 0.00666 -0.0878 0.4950 0.4462
0.500 0.3071 0.01402 0.00673 -0.0886 0.4917 0.4494
0.750 0.3387 0.01409 0.00683 -0.0894 0.4891 0.4522
1.000 0.3702 0.01411 0.00688 -0.0901 0.4869 0.4550
1.250 0.4018 0.01413 0.00693 -0.0909 0.4841 0.4580
1.500 0.4335 0.01417 0.00696 -0.0917 0.4812 0.4609
1.750 0.4652 0.01423 0.00698 -0.0925 0.4784 0.4634
2.000 0.4963 0.01419 0.00697 -0.0932 0.4757 0.4669
2.250 0.5273 0.01426 0.00705 -0.0939 0.4729 0.4699
2.500 0.5588 0.01447 0.00724 -0.0947 0.4696 0.4727
2.750 0.5897 0.01449 0.00732 -0.0953 0.4678 0.4756
3.000 0.6207 0.01453 0.00740 -0.0959 0.4653 0.4787
3.250 0.6517 0.01460 0.00747 -0.0965 0.4625 0.4817
3.500 0.6828 0.01468 0.00754 -0.0972 0.4598 0.4840
3.750 0.7133 0.01465 0.00756 -0.0977 0.4573 0.4877
4.000 0.7438 0.01472 0.00765 -0.0983 0.4548 0.4907
4.250 0.7745 0.01489 0.00781 -0.0988 0.4519 0.4937
4.500 0.8052 0.01508 0.00801 -0.0994 0.4491 0.4969
4.750 0.8351 0.01515 0.00813 -0.0998 0.4469 0.5002
5.000 0.8652 0.01524 0.00825 -0.1002 0.4445 0.5030
5.250 0.8953 0.01534 0.00835 -0.1007 0.4420 0.5054
5.500 0.9249 0.01534 0.00842 -0.1010 0.4394 0.5091
5.750 0.9544 0.01542 0.00854 -0.1013 0.4368 0.5123
6.000 0.9840 0.01557 0.00869 -0.1016 0.4342 0.5155
6.250 1.0144 0.01584 0.00893 -0.1022 0.4312 0.5189
6.500 1.0433 0.01600 0.00913 -0.1024 0.4291 0.5222
6.750 1.0716 0.01611 0.00929 -0.1025 0.4267 0.5249
7.000 1.0999 0.01619 0.00942 -0.1026 0.4241 0.5279
7.250 1.1280 0.01626 0.00956 -0.1026 0.4215 0.5315
7.500 1.1559 0.01638 0.00972 -0.1026 0.4189 0.5349
7.750 1.1837 0.01653 0.00989 -0.1026 0.4162 0.5384
8.000 1.2124 0.01677 0.01011 -0.1028 0.4131 0.5419
8.250 1.2399 0.01702 0.01038 -0.1027 0.4103 0.5451
8.500 1.2649 0.01715 0.01057 -0.1022 0.4077 0.5477
8.750 1.2898 0.01721 0.01072 -0.1017 0.4044 0.5515
9.000 1.3143 0.01732 0.01089 -0.1010 0.4010 0.5551
9.250 1.3385 0.01748 0.01108 -0.1004 0.3978 0.5588
9.500 1.3640 0.01775 0.01132 -0.1000 0.3941 0.5625
9.750 1.3847 0.01796 0.01159 -0.0987 0.3906 0.5660
10.000 1.4023 0.01813 0.01183 -0.0969 0.3865 0.5690
10.250 1.4171 0.01829 0.01204 -0.0946 0.3823 0.5721
10.500 1.4315 0.01852 0.01230 -0.0922 0.3786 0.5760
10.750 1.4508 0.01891 0.01268 -0.0908 0.3744 0.5798
11.000 1.4655 0.01930 0.01319 -0.0888 0.3710 0.5836
11.250 1.4814 0.01972 0.01370 -0.0870 0.3667 0.5875
11.500 1.4967 0.02023 0.01421 -0.0853 0.3622 0.5910
11.750 1.5109 0.02086 0.01480 -0.0835 0.3575 0.5941
12.000 1.5251 0.02146 0.01554 -0.0820 0.3532 0.5986
12.250 1.5386 0.02219 0.01637 -0.0805 0.3481 0.6025
12.500 1.5496 0.02312 0.01732 -0.0789 0.3430 0.6063
12.750 1.5595 0.02421 0.01843 -0.0773 0.3379 0.6104
13.000 1.5715 0.02530 0.01960 -0.0762 0.3323 0.6144
13.250 1.5797 0.02667 0.02101 -0.0750 0.3262 0.6183
13.500 1.5859 0.02825 0.02264 -0.0737 0.3204 0.6229
13.750 1.5939 0.02983 0.02433 -0.0728 0.3137 0.6271
14.000 1.5942 0.03200 0.02650 -0.0715 0.3066 0.6310
14.250 1.5980 0.03404 0.02861 -0.0706 0.2996 0.6351
14.500 1.5950 0.03664 0.03122 -0.0694 0.2916 0.6386
14.750 1.5919 0.03933 0.03396 -0.0685 0.2838 0.6427
15.000 1.5829 0.04260 0.03727 -0.0674 0.2748 0.6468
15.250 1.5749 0.04589 0.04062 -0.0665 0.2660 0.6510
15.500 1.5588 0.05001 0.04474 -0.0656 0.2566 0.6547
15.750 1.5492 0.05368 0.04845 -0.0650 0.2469 0.6588
16.000 1.5324 0.05810 0.05286 -0.0643 0.2373 0.6620
16.250 1.5152 0.06268 0.05746 -0.0639 0.2270 0.6656
16.500 1.5013 0.06700 0.06183 -0.0636 0.2170 0.6695
16.750 1.4835 0.07177 0.06660 -0.0633 0.2073 0.6732
17.000 1.4680 0.07639 0.07123 -0.0632 0.1976 0.6770
17.250 1.4541 0.08093 0.07577 -0.0633 0.1883 0.6810
17.500 1.4381 0.08575 0.08057 -0.0634 0.1795 0.6846
17.750 1.4266 0.09011 0.08495 -0.0637 0.1705 0.6890
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