AH 93-W-300 (ah93w300-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 93-W-300 (ah93w300-il) Reynolds number: 200,000 Max Cl/Cd: 42.24 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w300-il-200000.txt Download as CSV file: xf-ah93w300-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9808 0.10409 0.09764 -0.0472 1.0000 0.1543
-19.500 -1.0086 0.09741 0.09079 -0.0494 1.0000 0.1599
-19.250 -0.9778 0.09840 0.09197 -0.0491 1.0000 0.1633
-19.000 -0.9968 0.09297 0.08644 -0.0509 1.0000 0.1691
-18.750 -0.9786 0.09233 0.08591 -0.0510 1.0000 0.1732
-18.500 -0.9781 0.08943 0.08303 -0.0519 1.0000 0.1784
-18.250 -0.9820 0.08608 0.07966 -0.0528 1.0000 0.1838
-18.000 -0.9680 0.08488 0.07855 -0.0532 1.0000 0.1885
-17.750 -0.9886 0.07958 0.07315 -0.0545 1.0000 0.1951
-17.500 -0.9644 0.07964 0.07334 -0.0545 1.0000 0.1994
-17.250 -0.9983 0.07299 0.06653 -0.0561 1.0000 0.2068
-17.000 -0.9646 0.07412 0.06784 -0.0557 1.0000 0.2106
-16.750 -1.0025 0.06726 0.06080 -0.0571 1.0000 0.2183
-16.500 -0.9690 0.06834 0.06206 -0.0568 1.0000 0.2222
-16.250 -0.9636 0.06637 0.06011 -0.0571 1.0000 0.2278
-16.000 -0.9811 0.06207 0.05575 -0.0576 1.0000 0.2342
-15.750 -0.9544 0.06242 0.05622 -0.0574 1.0000 0.2383
-15.500 -1.0065 0.05500 0.04858 -0.0580 1.0000 0.2464
-15.250 -0.9643 0.05684 0.05062 -0.0575 1.0000 0.2498
-15.000 -0.9578 0.05535 0.04917 -0.0573 1.0000 0.2551
-14.750 -0.9919 0.05034 0.04403 -0.0568 1.0000 0.2618
-14.500 -0.9601 0.05126 0.04510 -0.0563 1.0000 0.2655
-14.250 -0.9802 0.04797 0.04177 -0.0552 1.0000 0.2715
-14.000 -1.0003 0.04507 0.03883 -0.0536 1.0000 0.2769
-13.750 -0.9749 0.04570 0.03960 -0.0527 1.0000 0.2806
-13.500 -1.0004 0.04332 0.03721 -0.0498 1.0000 0.2858
-13.250 -1.0907 0.03914 0.03287 -0.0421 0.9985 0.2903
-13.000 -1.0272 0.04053 0.03448 -0.0452 0.9959 0.2946
-12.750 -0.9945 0.03915 0.03310 -0.0493 0.9904 0.3005
-12.500 -0.9903 0.03555 0.02934 -0.0532 0.9793 0.3074
-12.250 -0.9319 0.03633 0.03028 -0.0567 0.9760 0.3117
-12.000 -0.9127 0.03427 0.02815 -0.0599 0.9655 0.3180
-11.750 -0.8903 0.03207 0.02586 -0.0639 0.9582 0.3243
-11.500 -0.8358 0.03300 0.02694 -0.0663 0.9497 0.3286
-11.250 -0.8216 0.03075 0.02456 -0.0693 0.9381 0.3354
-11.000 -0.8164 0.02902 0.02271 -0.0693 0.9202 0.3407
-10.750 -0.7586 0.02997 0.02379 -0.0718 0.9123 0.3441
-10.500 -0.7369 0.02968 0.02349 -0.0715 0.8960 0.3483
-10.250 -0.7744 0.02715 0.02064 -0.0673 0.8759 0.3543
-10.000 -0.7488 0.02685 0.02033 -0.0671 0.8640 0.3582
-9.750 -0.7095 0.02735 0.02091 -0.0676 0.8534 0.3614
-9.500 -0.6866 0.02730 0.02086 -0.0671 0.8406 0.3653
-9.250 -0.6838 0.02622 0.01954 -0.0656 0.8289 0.3709
-9.000 -0.6692 0.02561 0.01885 -0.0647 0.8175 0.3752
-8.750 -0.6336 0.02594 0.01928 -0.0649 0.8070 0.3782
-8.500 -0.6019 0.02615 0.01946 -0.0650 0.7972 0.3816
-8.250 -0.5833 0.02579 0.01905 -0.0644 0.7868 0.3861
-8.000 -0.5758 0.02472 0.01771 -0.0635 0.7762 0.3918
-7.750 -0.5421 0.02478 0.01782 -0.0637 0.7673 0.3947
-7.500 -0.5098 0.02506 0.01817 -0.0638 0.7581 0.3975
-7.250 -0.4818 0.02510 0.01823 -0.0637 0.7478 0.4009
-7.000 -0.4585 0.02476 0.01777 -0.0636 0.7387 0.4054
-6.750 -0.4408 0.02401 0.01673 -0.0637 0.7301 0.4110
-6.500 -0.4108 0.02396 0.01681 -0.0636 0.7210 0.4138
-6.250 -0.3797 0.02412 0.01702 -0.0636 0.7116 0.4165
-6.000 -0.3492 0.02425 0.01710 -0.0637 0.7031 0.4197
-5.750 -0.3230 0.02413 0.01695 -0.0638 0.6945 0.4238
-5.500 -0.3000 0.02357 0.01625 -0.0641 0.6854 0.4290
-5.250 -0.2726 0.02322 0.01580 -0.0643 0.6771 0.4328
-5.000 -0.2412 0.02344 0.01603 -0.0644 0.6689 0.4354
-4.750 -0.2123 0.02356 0.01624 -0.0642 0.6602 0.4383
-4.500 -0.1836 0.02354 0.01619 -0.0644 0.6517 0.4417
-4.250 -0.1552 0.02335 0.01586 -0.0648 0.6441 0.4463
-4.000 -0.1287 0.02296 0.01530 -0.0656 0.6361 0.4514
-3.750 -0.1004 0.02281 0.01522 -0.0656 0.6277 0.4544
-3.500 -0.0705 0.02291 0.01535 -0.0655 0.6201 0.4569
-3.250 -0.0395 0.02314 0.01551 -0.0657 0.6128 0.4599
-3.000 -0.0118 0.02315 0.01557 -0.0657 0.6051 0.4636
-2.750 0.0166 0.02297 0.01534 -0.0662 0.5972 0.4680
-2.500 0.0464 0.02268 0.01485 -0.0672 0.5903 0.4728
-2.250 0.0759 0.02260 0.01473 -0.0675 0.5834 0.4761
-2.000 0.1035 0.02269 0.01494 -0.0672 0.5760 0.4788
-1.750 0.1325 0.02278 0.01506 -0.0671 0.5688 0.4817
-1.500 0.1625 0.02284 0.01504 -0.0674 0.5623 0.4851
-1.250 0.1923 0.02290 0.01504 -0.0679 0.5558 0.4893
-1.000 0.2210 0.02276 0.01488 -0.0685 0.5489 0.4940
-0.750 0.2510 0.02253 0.01456 -0.0694 0.5423 0.4980
-0.500 0.2801 0.02248 0.01450 -0.0694 0.5362 0.5009
-0.250 0.3090 0.02270 0.01473 -0.0694 0.5301 0.5037
0.000 0.3362 0.02282 0.01494 -0.0691 0.5237 0.5069
0.250 0.3651 0.02287 0.01499 -0.0693 0.5174 0.5107
0.500 0.3957 0.02285 0.01487 -0.0699 0.5116 0.5149
0.750 0.4271 0.02292 0.01482 -0.0709 0.5057 0.5192
1.000 0.4555 0.02281 0.01472 -0.0714 0.4995 0.5231
1.250 0.4825 0.02274 0.01471 -0.0711 0.4933 0.5264
1.500 0.5109 0.02284 0.01480 -0.0710 0.4877 0.5294
1.750 0.5410 0.02310 0.01501 -0.0713 0.4820 0.5326
2.000 0.5667 0.02317 0.01517 -0.0710 0.4760 0.5362
2.250 0.5948 0.02322 0.01521 -0.0711 0.4698 0.5405
2.500 0.6253 0.02325 0.01516 -0.0718 0.4643 0.5450
2.750 0.6583 0.02348 0.01522 -0.0730 0.4585 0.5488
3.000 0.6822 0.02331 0.01518 -0.0725 0.4528 0.5525
3.250 0.7076 0.02339 0.01533 -0.0719 0.4469 0.5557
3.500 0.7348 0.02352 0.01545 -0.0717 0.4414 0.5591
3.750 0.7658 0.02385 0.01568 -0.0722 0.4359 0.5630
4.000 0.7883 0.02396 0.01591 -0.0714 0.4303 0.5671
4.250 0.8147 0.02404 0.01599 -0.0713 0.4243 0.5713
4.500 0.8438 0.02413 0.01599 -0.0717 0.4189 0.5754
4.750 0.8758 0.02433 0.01605 -0.0728 0.4134 0.5794
5.000 0.8950 0.02437 0.01626 -0.0713 0.4079 0.5832
5.250 0.9174 0.02452 0.01648 -0.0704 0.4022 0.5867
5.500 0.9430 0.02467 0.01660 -0.0699 0.3970 0.5904
5.750 0.9719 0.02498 0.01684 -0.0702 0.3917 0.5944
6.000 0.9896 0.02520 0.01718 -0.0687 0.3862 0.5987
6.250 1.0121 0.02539 0.01736 -0.0680 0.3805 0.6033
6.500 1.0391 0.02560 0.01747 -0.0681 0.3754 0.6074
6.750 1.0638 0.02579 0.01764 -0.0679 0.3702 0.6116
7.000 1.0771 0.02602 0.01801 -0.0657 0.3648 0.6153
7.250 1.0942 0.02625 0.01829 -0.0640 0.3595 0.6190
7.500 1.1181 0.02651 0.01847 -0.0634 0.3546 0.6233
7.750 1.1298 0.02691 0.01894 -0.0609 0.3497 0.6278
8.000 1.1374 0.02734 0.01944 -0.0580 0.3444 0.6323
8.250 1.1549 0.02775 0.01983 -0.0569 0.3393 0.6368
8.500 1.1865 0.02809 0.01997 -0.0578 0.3340 0.6406
8.750 1.1897 0.02874 0.02082 -0.0548 0.3290 0.6450
9.000 1.2005 0.02936 0.02154 -0.0528 0.3237 0.6491
9.250 1.2181 0.02985 0.02201 -0.0517 0.3188 0.6538
9.500 1.2350 0.03054 0.02269 -0.0507 0.3138 0.6588
9.750 1.2406 0.03156 0.02383 -0.0487 0.3084 0.6636
10.000 1.2540 0.03235 0.02461 -0.0477 0.3033 0.6684
10.250 1.2811 0.03280 0.02487 -0.0480 0.2982 0.6727
10.500 1.2793 0.03417 0.02648 -0.0457 0.2933 0.6773
10.750 1.2866 0.03529 0.02768 -0.0442 0.2882 0.6819
11.000 1.3040 0.03600 0.02832 -0.0435 0.2835 0.6874
11.250 1.3113 0.03736 0.02976 -0.0423 0.2786 0.6929
11.500 1.3149 0.03898 0.03147 -0.0412 0.2735 0.6983
11.750 1.3279 0.04014 0.03257 -0.0408 0.2688 0.7033
12.000 1.3433 0.04103 0.03346 -0.0402 0.2643 0.7088
12.250 1.3397 0.04321 0.03583 -0.0388 0.2595 0.7137
12.500 1.3459 0.04480 0.03746 -0.0381 0.2550 0.7197
12.750 1.3684 0.04534 0.03785 -0.0379 0.2507 0.7271
13.000 1.3623 0.04811 0.04080 -0.0372 0.2462 0.7326
13.250 1.3634 0.05019 0.04300 -0.0365 0.2417 0.7384
13.500 1.3745 0.05151 0.04431 -0.0360 0.2377 0.7450
13.750 1.3834 0.05317 0.04598 -0.0356 0.2336 0.7522
14.000 1.3773 0.05633 0.04929 -0.0355 0.2292 0.7589
14.250 1.3827 0.05829 0.05130 -0.0352 0.2252 0.7660
14.500 1.4050 0.05856 0.05146 -0.0347 0.2215 0.7751
14.750 1.3907 0.06268 0.05581 -0.0347 0.2175 0.7823
15.000 1.3892 0.06559 0.05882 -0.0348 0.2134 0.7901
15.250 1.3987 0.06712 0.06036 -0.0345 0.2100 0.7990
15.500 1.4085 0.06885 0.06208 -0.0344 0.2064 0.8094
15.750 1.3939 0.07326 0.06671 -0.0348 0.2025 0.8170
16.000 1.3958 0.07574 0.06925 -0.0348 0.1989 0.8278
16.250 1.4143 0.07622 0.06965 -0.0342 0.1958 0.8415
16.500 1.4020 0.08041 0.07402 -0.0346 0.1923 0.8528
16.750 1.3900 0.08454 0.07833 -0.0349 0.1886 0.8647
17.000 1.3948 0.08646 0.08027 -0.0346 0.1855 0.8819
17.250 1.4164 0.08559 0.07928 -0.0326 0.1828 0.9087
17.500 1.3823 0.09180 0.08580 -0.0329 0.1795 0.9335
17.750 1.3667 0.09569 0.08983 -0.0335 0.1760 1.0000
18.000 1.3857 0.09715 0.09118 -0.0350 0.1730 1.0000
18.250 1.4071 0.09800 0.09190 -0.0358 0.1702 1.0000
18.500 1.3684 0.10667 0.10087 -0.0392 0.1662 1.0000
18.750 1.3727 0.10968 0.10388 -0.0408 0.1631 1.0000
19.000 1.4010 0.10931 0.10334 -0.0409 0.1608 1.0000
19.250 1.3794 0.11573 0.10993 -0.0437 0.1574 1.0000
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