AH 94-156 (ah94156-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 94-156 (ah94156-il) Reynolds number: 500,000 Max Cl/Cd: 95.23 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah94156-il-500000-n5.txt Download as CSV file: xf-ah94156-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 94-156
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.5038 0.05373 0.05022 -0.1036 0.7867 0.0083
-12.500 -0.5442 0.04553 0.04174 -0.1082 0.7831 0.0083
-12.250 -0.5686 0.04115 0.03714 -0.1083 0.7798 0.0083
-12.000 -0.5878 0.03778 0.03352 -0.1067 0.7769 0.0083
-11.750 -0.6006 0.03511 0.03061 -0.1045 0.7743 0.0083
-11.500 -0.6107 0.03269 0.02797 -0.1018 0.7714 0.0084
-11.250 -0.6198 0.03047 0.02553 -0.0986 0.7686 0.0085
-11.000 -0.6197 0.02907 0.02400 -0.0958 0.7659 0.0087
-10.750 -0.6166 0.02792 0.02270 -0.0930 0.7633 0.0088
-10.500 -0.6112 0.02667 0.02123 -0.0904 0.7610 0.0088
-10.250 -0.5973 0.02596 0.02046 -0.0889 0.7588 0.0091
-10.000 -0.5841 0.02486 0.01920 -0.0874 0.7566 0.0092
-9.750 -0.5694 0.02377 0.01796 -0.0860 0.7545 0.0093
-9.500 -0.5526 0.02282 0.01685 -0.0848 0.7523 0.0096
-9.250 -0.5349 0.02181 0.01568 -0.0837 0.7502 0.0098
-9.000 -0.5157 0.02094 0.01464 -0.0827 0.7482 0.0101
-8.750 -0.4950 0.02023 0.01376 -0.0819 0.7463 0.0105
-8.500 -0.4740 0.01942 0.01279 -0.0812 0.7445 0.0108
-8.250 -0.4516 0.01879 0.01204 -0.0806 0.7427 0.0111
-8.000 -0.4308 0.01786 0.01102 -0.0798 0.7408 0.0114
-7.750 -0.4085 0.01723 0.01034 -0.0793 0.7387 0.0118
-7.500 -0.3855 0.01669 0.00974 -0.0788 0.7367 0.0121
-7.250 -0.3619 0.01620 0.00918 -0.0783 0.7347 0.0125
-7.000 -0.3383 0.01573 0.00863 -0.0779 0.7329 0.0130
-6.750 -0.3144 0.01526 0.00809 -0.0774 0.7314 0.0135
-6.500 -0.2904 0.01483 0.00757 -0.0770 0.7298 0.0139
-6.250 -0.2660 0.01441 0.00710 -0.0766 0.7280 0.0144
-6.000 -0.2422 0.01396 0.00664 -0.0763 0.7260 0.0153
-5.750 -0.2172 0.01363 0.00630 -0.0760 0.7239 0.0162
-5.500 -0.1920 0.01332 0.00595 -0.0758 0.7219 0.0172
-5.250 -0.1667 0.01301 0.00559 -0.0755 0.7202 0.0181
-5.000 -0.1417 0.01267 0.00521 -0.0752 0.7185 0.0193
-4.750 -0.1162 0.01240 0.00491 -0.0750 0.7167 0.0207
-4.250 -0.0643 0.01192 0.00439 -0.0747 0.7131 0.0252
-4.000 -0.0380 0.01172 0.00419 -0.0747 0.7111 0.0287
-3.750 -0.0119 0.01148 0.00398 -0.0746 0.7089 0.0335
-3.500 0.0144 0.01128 0.00378 -0.0745 0.7069 0.0408
-3.250 0.0406 0.01106 0.00360 -0.0744 0.7049 0.0537
-3.000 0.0665 0.01081 0.00343 -0.0743 0.7030 0.0759
-2.750 0.0920 0.01052 0.00326 -0.0742 0.7012 0.1157
-2.500 0.1167 0.01017 0.00312 -0.0740 0.6995 0.1776
-2.250 0.1405 0.00974 0.00301 -0.0737 0.6972 0.2615
-2.000 0.1632 0.00921 0.00288 -0.0733 0.6947 0.3727
-1.750 0.1847 0.00860 0.00274 -0.0726 0.6921 0.5045
-1.500 0.2043 0.00792 0.00262 -0.0714 0.6898 0.6560
-1.250 0.2241 0.00801 0.00320 -0.0690 0.6876 0.7829
-1.000 0.2525 0.00818 0.00328 -0.0691 0.6853 0.8109
-0.750 0.2801 0.00832 0.00341 -0.0690 0.6824 0.8222
-0.500 0.3077 0.00845 0.00351 -0.0690 0.6790 0.8312
-0.250 0.3349 0.00861 0.00364 -0.0688 0.6758 0.8393
0.000 0.3622 0.00873 0.00372 -0.0687 0.6730 0.8456
0.250 0.3892 0.00888 0.00382 -0.0683 0.6705 0.8504
0.500 0.4164 0.00897 0.00391 -0.0683 0.6670 0.8558
0.750 0.4436 0.00902 0.00395 -0.0683 0.6634 0.8596
1.000 0.4702 0.00909 0.00401 -0.0681 0.6601 0.8622
1.250 0.4974 0.00914 0.00402 -0.0680 0.6570 0.8649
1.500 0.5248 0.00918 0.00405 -0.0681 0.6535 0.8674
1.750 0.5526 0.00920 0.00407 -0.0683 0.6495 0.8697
2.000 0.5808 0.00922 0.00407 -0.0687 0.6455 0.8717
2.250 0.6090 0.00923 0.00405 -0.0690 0.6420 0.8733
2.500 0.6360 0.00924 0.00408 -0.0691 0.6380 0.8742
2.750 0.6628 0.00925 0.00410 -0.0691 0.6329 0.8753
3.000 0.6898 0.00927 0.00410 -0.0691 0.6280 0.8762
3.250 0.7167 0.00930 0.00415 -0.0692 0.6227 0.8773
3.500 0.7435 0.00933 0.00418 -0.0693 0.6168 0.8783
3.750 0.7702 0.00937 0.00420 -0.0693 0.6112 0.8792
4.000 0.7967 0.00941 0.00427 -0.0694 0.6039 0.8802
4.250 0.8226 0.00947 0.00431 -0.0693 0.5963 0.8813
4.500 0.8485 0.00953 0.00438 -0.0692 0.5873 0.8821
4.750 0.8740 0.00961 0.00445 -0.0691 0.5785 0.8829
5.000 0.8983 0.00972 0.00454 -0.0687 0.5678 0.8840
5.250 0.9221 0.00984 0.00464 -0.0683 0.5549 0.8850
5.500 0.9454 0.00998 0.00477 -0.0678 0.5422 0.8857
5.750 0.9675 0.01016 0.00492 -0.0671 0.5288 0.8864
6.000 0.9879 0.01038 0.00510 -0.0661 0.5136 0.8873
6.250 1.0059 0.01061 0.00529 -0.0646 0.4985 0.8882
6.500 1.0221 0.01087 0.00551 -0.0627 0.4829 0.8889
6.750 1.0358 0.01113 0.00576 -0.0604 0.4685 0.8897
7.000 1.0463 0.01143 0.00603 -0.0575 0.4543 0.8907
7.250 1.0573 0.01181 0.00639 -0.0549 0.4406 0.8916
7.500 1.0668 0.01228 0.00683 -0.0521 0.4256 0.8930
7.750 1.0735 0.01289 0.00738 -0.0490 0.4073 0.8943
8.250 1.0861 0.01437 0.00874 -0.0433 0.3682 0.8965
8.500 1.0935 0.01518 0.00948 -0.0409 0.3492 0.8975
8.750 1.0987 0.01613 0.01035 -0.0383 0.3284 0.8985
9.000 1.1062 0.01705 0.01121 -0.0360 0.3079 0.8994
9.250 1.1113 0.01812 0.01219 -0.0337 0.2852 0.9003
9.500 1.1159 0.01928 0.01324 -0.0313 0.2604 0.9013
9.750 1.1196 0.02048 0.01433 -0.0289 0.2365 0.9024
10.000 1.1226 0.02179 0.01552 -0.0266 0.2109 0.9033
10.250 1.1266 0.02308 0.01671 -0.0244 0.1858 0.9041
10.500 1.1293 0.02451 0.01800 -0.0223 0.1593 0.9049
10.750 1.1336 0.02590 0.01929 -0.0204 0.1371 0.9057
11.000 1.1370 0.02741 0.02068 -0.0186 0.1139 0.9066
11.250 1.1426 0.02883 0.02203 -0.0170 0.0949 0.9074
11.500 1.1468 0.03040 0.02351 -0.0155 0.0772 0.9082
11.750 1.1510 0.03204 0.02506 -0.0140 0.0603 0.9090
12.000 1.1597 0.03340 0.02642 -0.0130 0.0522 0.9097
12.250 1.1666 0.03493 0.02792 -0.0120 0.0427 0.9105
12.500 1.1738 0.03649 0.02948 -0.0110 0.0352 0.9113
12.750 1.1825 0.03798 0.03099 -0.0103 0.0299 0.9120
13.000 1.1903 0.03958 0.03261 -0.0095 0.0253 0.9128
13.250 1.1971 0.04131 0.03434 -0.0088 0.0212 0.9136
13.500 1.2050 0.04298 0.03606 -0.0082 0.0182 0.9143
13.750 1.2125 0.04474 0.03785 -0.0077 0.0162 0.9150
14.250 1.2262 0.04847 0.04171 -0.0067 0.0132 0.9166
14.500 1.2335 0.05035 0.04367 -0.0064 0.0122 0.9176
14.750 1.2396 0.05240 0.04579 -0.0061 0.0112 0.9187
15.000 1.2453 0.05455 0.04801 -0.0059 0.0106 0.9198
15.250 1.2485 0.05702 0.05055 -0.0058 0.0098 0.9210
15.500 1.2538 0.05932 0.05295 -0.0057 0.0095 0.9221
15.750 1.2594 0.06164 0.05536 -0.0059 0.0091 0.9231
16.000 1.2628 0.06429 0.05810 -0.0060 0.0086 0.9242
16.250 1.2657 0.06705 0.06095 -0.0063 0.0082 0.9253
16.500 1.2678 0.06998 0.06397 -0.0067 0.0077 0.9265
16.750 1.2699 0.07298 0.06705 -0.0073 0.0076 0.9276
17.000 1.2688 0.07649 0.07066 -0.0079 0.0072 0.9287
17.500 1.2721 0.08304 0.07744 -0.0097 0.0068 0.9315
17.750 1.2724 0.08658 0.08109 -0.0108 0.0065 0.9331
18.000 1.2711 0.09042 0.08504 -0.0120 0.0065 0.9348
18.250 1.2712 0.09412 0.08885 -0.0133 0.0063 0.9368
18.500 1.2704 0.09803 0.09287 -0.0148 0.0060 0.9390
18.750 1.2685 0.10221 0.09716 -0.0165 0.0059 0.9412
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