AH 94-W-301 (ah94w301-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 94-W-301 (ah94w301-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.96 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah94w301-il-1000000.txt Download as CSV file: xf-ah94w301-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.1912 0.09373 0.08974 -0.0292 1.0000 0.1562
-19.000 -1.1965 0.09031 0.08634 -0.0300 1.0000 0.1601
-18.750 -1.1969 0.08745 0.08347 -0.0307 1.0000 0.1635
-18.500 -1.1970 0.08463 0.08061 -0.0314 1.0000 0.1663
-18.250 -1.1931 0.08226 0.07823 -0.0320 1.0000 0.1692
-18.000 -1.2000 0.07877 0.07475 -0.0327 1.0000 0.1735
-17.750 -1.2023 0.07580 0.07176 -0.0332 1.0000 0.1770
-17.500 -1.1960 0.07375 0.06969 -0.0337 1.0000 0.1798
-17.250 -1.1970 0.07099 0.06691 -0.0341 1.0000 0.1833
-17.000 -1.2032 0.06770 0.06363 -0.0345 1.0000 0.1873
-16.750 -1.2009 0.06533 0.06126 -0.0349 1.0000 0.1908
-16.500 -1.1976 0.06304 0.05892 -0.0352 1.0000 0.1937
-16.250 -1.1999 0.06030 0.05619 -0.0354 1.0000 0.1978
-16.000 -1.2036 0.05743 0.05333 -0.0355 1.0000 0.2018
-15.750 -1.2021 0.05510 0.05098 -0.0357 1.0000 0.2054
-15.500 -1.1933 0.05347 0.04932 -0.0358 1.0000 0.2079
-15.250 -1.2000 0.05048 0.04633 -0.0357 1.0000 0.2122
-15.000 -1.2008 0.04807 0.04394 -0.0356 1.0000 0.2161
-14.750 -1.1986 0.04598 0.04183 -0.0354 1.0000 0.2196
-14.500 -1.1859 0.04419 0.04000 -0.0365 0.9991 0.2225
-14.250 -1.1398 0.04054 0.03632 -0.0471 0.9355 0.2288
-14.000 -1.1221 0.03843 0.03379 -0.0501 0.8313 0.2331
-13.750 -1.1123 0.03711 0.03231 -0.0500 0.7989 0.2362
-13.500 -1.1063 0.03537 0.03047 -0.0500 0.7774 0.2396
-13.250 -1.1071 0.03312 0.02817 -0.0498 0.7602 0.2441
-12.750 -1.0918 0.03000 0.02489 -0.0498 0.7297 0.2514
-12.500 -1.0847 0.02846 0.02327 -0.0497 0.7162 0.2548
-12.250 -1.0835 0.02651 0.02129 -0.0493 0.7047 0.2593
-12.000 -1.0766 0.02496 0.01968 -0.0491 0.6932 0.2633
-11.750 -1.0636 0.02382 0.01849 -0.0492 0.6838 0.2666
-11.500 -1.0503 0.02274 0.01733 -0.0492 0.6735 0.2696
-11.250 -1.0465 0.02098 0.01557 -0.0488 0.6656 0.2744
-11.000 -1.0361 0.01970 0.01425 -0.0487 0.6572 0.2783
-10.750 -1.0214 0.01877 0.01325 -0.0486 0.6477 0.2817
-10.500 -1.0031 0.01803 0.01246 -0.0487 0.6410 0.2843
-10.250 -1.0014 0.01671 0.01112 -0.0471 0.6339 0.2884
-10.000 -0.9862 0.01570 0.01006 -0.0475 0.6261 0.2924
-9.750 -0.9630 0.01501 0.00934 -0.0487 0.6201 0.2962
-9.500 -0.9360 0.01455 0.00883 -0.0500 0.6144 0.2993
-9.250 -0.9083 0.01413 0.00835 -0.0513 0.6081 0.3023
-9.000 -0.8819 0.01365 0.00784 -0.0525 0.6008 0.3067
-8.750 -0.8532 0.01331 0.00751 -0.0536 0.5964 0.3106
-8.500 -0.8235 0.01309 0.00726 -0.0546 0.5912 0.3140
-8.250 -0.7934 0.01295 0.00706 -0.0556 0.5856 0.3166
-8.000 -0.7638 0.01274 0.00680 -0.0567 0.5796 0.3200
-7.750 -0.7338 0.01247 0.00654 -0.0579 0.5753 0.3242
-7.500 -0.7028 0.01227 0.00635 -0.0590 0.5716 0.3277
-7.250 -0.6716 0.01214 0.00619 -0.0601 0.5671 0.3310
-7.000 -0.6404 0.01206 0.00605 -0.0612 0.5622 0.3335
-6.750 -0.6095 0.01195 0.00589 -0.0622 0.5565 0.3365
-6.500 -0.5781 0.01175 0.00571 -0.0634 0.5529 0.3407
-6.250 -0.5461 0.01160 0.00557 -0.0646 0.5500 0.3442
-6.000 -0.5142 0.01150 0.00546 -0.0658 0.5463 0.3473
-5.750 -0.4823 0.01144 0.00536 -0.0668 0.5423 0.3500
-5.500 -0.4505 0.01142 0.00527 -0.0678 0.5379 0.3520
-5.250 -0.4190 0.01129 0.00514 -0.0690 0.5325 0.3564
-5.000 -0.3865 0.01115 0.00503 -0.0702 0.5303 0.3599
-4.750 -0.3541 0.01107 0.00495 -0.0714 0.5276 0.3632
-4.500 -0.3217 0.01101 0.00488 -0.0725 0.5244 0.3661
-4.250 -0.2895 0.01098 0.00481 -0.0735 0.5211 0.3684
-4.000 -0.2574 0.01095 0.00474 -0.0745 0.5175 0.3709
-3.750 -0.2254 0.01087 0.00466 -0.0756 0.5129 0.3751
-3.500 -0.1930 0.01081 0.00461 -0.0768 0.5100 0.3784
-3.250 -0.1602 0.01075 0.00456 -0.0779 0.5076 0.3814
-3.000 -0.1277 0.01072 0.00452 -0.0790 0.5049 0.3840
-2.750 -0.0952 0.01071 0.00448 -0.0800 0.5019 0.3863
-2.500 -0.0629 0.01069 0.00444 -0.0810 0.4988 0.3887
-2.250 -0.0307 0.01063 0.00439 -0.0820 0.4954 0.3929
-2.000 0.0012 0.01064 0.00438 -0.0830 0.4912 0.3961
-1.750 0.0338 0.01062 0.00437 -0.0841 0.4891 0.3990
-1.500 0.0665 0.01059 0.00435 -0.0851 0.4870 0.4018
-1.250 0.0990 0.01059 0.00434 -0.0861 0.4844 0.4042
-1.000 0.1314 0.01060 0.00433 -0.0870 0.4815 0.4060
-0.750 0.1637 0.01054 0.00429 -0.0880 0.4786 0.4101
-0.500 0.1959 0.01054 0.00429 -0.0890 0.4755 0.4136
-0.250 0.2276 0.01059 0.00433 -0.0898 0.4718 0.4167
0.000 0.2596 0.01063 0.00436 -0.0907 0.4691 0.4195
0.250 0.2921 0.01063 0.00437 -0.0916 0.4674 0.4220
0.500 0.3245 0.01064 0.00438 -0.0925 0.4651 0.4240
0.750 0.3568 0.01063 0.00438 -0.0934 0.4625 0.4269
1.000 0.3890 0.01061 0.00438 -0.0944 0.4597 0.4309
1.250 0.4208 0.01063 0.00442 -0.0952 0.4569 0.4340
1.500 0.4523 0.01070 0.00447 -0.0959 0.4537 0.4368
1.750 0.4832 0.01082 0.00455 -0.0966 0.4499 0.4394
2.000 0.5154 0.01083 0.00458 -0.0974 0.4485 0.4417
2.250 0.5475 0.01086 0.00462 -0.0982 0.4465 0.4437
2.500 0.5795 0.01085 0.00464 -0.0990 0.4442 0.4473
2.750 0.6114 0.01085 0.00468 -0.0998 0.4416 0.4510
3.000 0.6428 0.01090 0.00474 -0.1005 0.4391 0.4539
3.250 0.6738 0.01097 0.00481 -0.1011 0.4363 0.4567
3.500 0.7043 0.01109 0.00491 -0.1016 0.4329 0.4593
3.750 0.7350 0.01120 0.00501 -0.1021 0.4299 0.4618
4.000 0.7665 0.01125 0.00507 -0.1028 0.4282 0.4636
4.250 0.7980 0.01125 0.00512 -0.1035 0.4262 0.4677
4.500 0.8293 0.01128 0.00520 -0.1041 0.4240 0.4712
4.750 0.8602 0.01134 0.00528 -0.1047 0.4215 0.4742
5.000 0.8906 0.01143 0.00537 -0.1051 0.4188 0.4772
5.250 0.9203 0.01155 0.00549 -0.1055 0.4158 0.4800
5.500 0.9493 0.01174 0.00564 -0.1057 0.4123 0.4824
5.750 0.9797 0.01183 0.00575 -0.1061 0.4104 0.4841
6.000 1.0104 0.01184 0.00583 -0.1066 0.4086 0.4884
6.250 1.0409 0.01190 0.00594 -0.1071 0.4064 0.4919
6.500 1.0709 0.01197 0.00605 -0.1074 0.4040 0.4952
6.750 1.1002 0.01208 0.00618 -0.1077 0.4014 0.4983
7.000 1.1288 0.01222 0.00631 -0.1077 0.3985 0.5012
7.250 1.1562 0.01242 0.00649 -0.1076 0.3950 0.5034
7.500 1.1844 0.01258 0.00666 -0.1076 0.3921 0.5054
7.750 1.2140 0.01261 0.00676 -0.1079 0.3899 0.5099
8.000 1.2430 0.01268 0.00689 -0.1081 0.3870 0.5135
8.250 1.2709 0.01280 0.00703 -0.1080 0.3836 0.5170
8.500 1.2973 0.01297 0.00720 -0.1077 0.3802 0.5202
8.750 1.3212 0.01323 0.00743 -0.1070 0.3757 0.5230
9.000 1.3484 0.01334 0.00758 -0.1068 0.3722 0.5252
9.250 1.3754 0.01344 0.00772 -0.1065 0.3681 0.5283
9.500 1.4002 0.01360 0.00791 -0.1060 0.3641 0.5326
9.750 1.4217 0.01385 0.00817 -0.1048 0.3597 0.5362
10.000 1.4434 0.01410 0.00845 -0.1037 0.3557 0.5398
10.250 1.4654 0.01425 0.00865 -0.1025 0.3521 0.5431
10.500 1.4829 0.01450 0.00891 -0.1006 0.3476 0.5458
10.750 1.4999 0.01490 0.00929 -0.0987 0.3425 0.5478
11.000 1.5191 0.01526 0.00969 -0.0972 0.3378 0.5522
11.250 1.5414 0.01555 0.01003 -0.0964 0.3331 0.5564
11.500 1.5592 0.01600 0.01050 -0.0948 0.3273 0.5603
11.750 1.5734 0.01661 0.01112 -0.0928 0.3213 0.5639
12.000 1.5928 0.01706 0.01160 -0.0917 0.3157 0.5672
12.250 1.6056 0.01782 0.01234 -0.0897 0.3087 0.5697
12.500 1.6187 0.01862 0.01316 -0.0880 0.3021 0.5736
12.750 1.6309 0.01955 0.01412 -0.0864 0.2941 0.5781
13.000 1.6383 0.02084 0.01542 -0.0845 0.2859 0.5819
13.250 1.6451 0.02230 0.01689 -0.0829 0.2765 0.5855
13.500 1.6492 0.02405 0.01865 -0.0812 0.2674 0.5889
13.750 1.6470 0.02641 0.02098 -0.0795 0.2572 0.5916
14.000 1.6472 0.02868 0.02326 -0.0781 0.2471 0.5947
14.250 1.6402 0.03159 0.02619 -0.0765 0.2370 0.5994
14.500 1.6273 0.03509 0.02970 -0.0748 0.2261 0.6030
14.750 1.6169 0.03845 0.03308 -0.0734 0.2161 0.6064
15.000 1.5995 0.04247 0.03711 -0.0719 0.2063 0.6094
15.250 1.5813 0.04671 0.04136 -0.0706 0.1967 0.6121
15.500 1.5666 0.05075 0.04541 -0.0696 0.1877 0.6145
15.750 1.5473 0.05534 0.05000 -0.0686 0.1792 0.6163
16.000 1.5318 0.05970 0.05439 -0.0680 0.1706 0.6203
16.250 1.5165 0.06408 0.05881 -0.0675 0.1628 0.6239
16.500 1.5008 0.06857 0.06331 -0.0670 0.1551 0.6274
16.750 1.4911 0.07252 0.06729 -0.0668 0.1480 0.6311
17.000 1.4749 0.07720 0.07198 -0.0666 0.1411 0.6343
17.250 1.4690 0.08079 0.07558 -0.0665 0.1344 0.6377
17.500 1.4557 0.08531 0.08010 -0.0665 0.1284 0.6403
17.750 1.4499 0.08899 0.08381 -0.0667 0.1218 0.6454
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