AH 79-K-132/20 (ah79k132-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 79-K-132/20 (ah79k132-il) Reynolds number: 200,000 Max Cl/Cd: 78.38 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah79k132-il-200000-n5.txt Download as CSV file: xf-ah79k132-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 79-K-132/20
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.000 -0.1710 0.10713 0.10286 -0.0710 0.8015 0.0167
-11.750 -0.1708 0.10290 0.09864 -0.0727 0.8008 0.0165
-11.250 -0.2351 0.09777 0.09320 -0.0841 0.8043 0.0156
-11.000 -0.2275 0.09570 0.09114 -0.0851 0.8035 0.0162
-10.750 -0.2311 0.09075 0.08624 -0.0872 0.8026 0.0160
-10.500 -0.2212 0.08938 0.08487 -0.0880 0.8015 0.0175
-10.250 -0.2268 0.08433 0.07988 -0.0902 0.8004 0.0170
-10.000 -0.2267 0.08082 0.07641 -0.0919 0.7989 0.0178
-9.750 -0.2342 0.07583 0.07146 -0.0943 0.7974 0.0176
-9.500 -0.2458 0.07022 0.06592 -0.0976 0.7960 0.0174
-9.250 -0.2720 0.06243 0.05817 -0.1030 0.7943 0.0169
-9.000 -0.3043 0.05609 0.05176 -0.1036 0.7926 0.0166
-8.750 -0.3472 0.04811 0.04354 -0.1010 0.7905 0.0161
-8.500 -0.3740 0.04104 0.03606 -0.0977 0.7883 0.0160
-8.250 -0.3796 0.03700 0.03163 -0.0950 0.7865 0.0161
-8.000 -0.3768 0.03376 0.02800 -0.0927 0.7846 0.0164
-7.750 -0.3672 0.03132 0.02519 -0.0908 0.7829 0.0168
-7.500 -0.3539 0.02912 0.02262 -0.0892 0.7815 0.0173
-7.250 -0.3372 0.02730 0.02045 -0.0879 0.7802 0.0181
-7.000 -0.3183 0.02564 0.01844 -0.0867 0.7790 0.0188
-6.750 -0.2976 0.02421 0.01673 -0.0858 0.7774 0.0198
-6.500 -0.2749 0.02338 0.01564 -0.0851 0.7756 0.0213
-6.250 -0.2534 0.02222 0.01436 -0.0844 0.7737 0.0228
-6.000 -0.2303 0.02154 0.01361 -0.0839 0.7717 0.0242
-5.750 -0.2067 0.02083 0.01278 -0.0833 0.7700 0.0259
-5.500 -0.1828 0.02013 0.01195 -0.0827 0.7685 0.0281
-5.250 -0.1589 0.01949 0.01118 -0.0820 0.7670 0.0307
-5.000 -0.1348 0.01907 0.01072 -0.0816 0.7656 0.0355
-4.750 -0.1102 0.01872 0.01027 -0.0811 0.7641 0.0405
-4.500 -0.0875 0.01830 0.00988 -0.0805 0.7615 0.0455
-4.250 -0.0632 0.01808 0.00961 -0.0800 0.7590 0.0512
-4.000 -0.0386 0.01785 0.00938 -0.0796 0.7569 0.0584
-3.750 -0.0131 0.01769 0.00912 -0.0793 0.7549 0.0659
-3.500 0.0109 0.01729 0.00872 -0.0788 0.7532 0.0725
-3.250 0.0364 0.01705 0.00840 -0.0784 0.7517 0.0801
-3.000 0.0599 0.01677 0.00817 -0.0779 0.7493 0.0883
-2.750 0.0834 0.01661 0.00802 -0.0773 0.7461 0.0981
-2.500 0.1077 0.01639 0.00783 -0.0769 0.7434 0.1129
-2.250 0.1322 0.01610 0.00764 -0.0765 0.7413 0.1435
-2.000 0.1557 0.01561 0.00743 -0.0760 0.7394 0.2187
-1.750 0.1760 0.01482 0.00719 -0.0750 0.7379 0.3772
-1.500 0.1834 0.01380 0.00746 -0.0710 0.7341 0.6931
-1.250 0.2018 0.01403 0.00801 -0.0679 0.7307 0.8037
-1.000 0.2238 0.01420 0.00813 -0.0663 0.7280 0.8426
-0.750 0.2471 0.01429 0.00815 -0.0649 0.7260 0.8639
-0.500 0.2707 0.01436 0.00814 -0.0634 0.7243 0.8814
-0.250 0.2870 0.01461 0.00839 -0.0606 0.7201 0.9032
0.000 0.3102 0.01475 0.00853 -0.0589 0.7163 0.9214
0.250 0.3360 0.01470 0.00843 -0.0582 0.7136 0.9319
0.500 0.3715 0.01459 0.00824 -0.0595 0.7117 0.9374
0.750 0.4003 0.01443 0.00802 -0.0596 0.7099 0.9436
1.000 0.4265 0.01455 0.00816 -0.0598 0.7039 0.9476
1.250 0.4573 0.01446 0.00803 -0.0606 0.7006 0.9502
1.500 0.4880 0.01429 0.00782 -0.0612 0.6981 0.9531
1.750 0.5171 0.01409 0.00758 -0.0615 0.6961 0.9561
2.000 0.5399 0.01422 0.00776 -0.0611 0.6891 0.9597
2.250 0.5726 0.01407 0.00760 -0.0622 0.6858 0.9614
2.500 0.6055 0.01386 0.00737 -0.0633 0.6832 0.9631
2.750 0.6323 0.01395 0.00752 -0.0636 0.6766 0.9661
3.000 0.6615 0.01381 0.00739 -0.0640 0.6723 0.9688
3.250 0.6911 0.01359 0.00716 -0.0644 0.6693 0.9715
3.500 0.7215 0.01369 0.00734 -0.0655 0.6615 0.9736
3.750 0.7550 0.01351 0.00719 -0.0667 0.6569 0.9753
4.000 0.7847 0.01351 0.00725 -0.0675 0.6492 0.9776
4.250 0.8159 0.01333 0.00709 -0.0683 0.6430 0.9795
4.500 0.8438 0.01332 0.00713 -0.0686 0.6337 0.9824
4.750 0.8744 0.01317 0.00703 -0.0693 0.6258 0.9844
5.000 0.9060 0.01308 0.00697 -0.0703 0.6160 0.9860
5.250 0.9362 0.01306 0.00698 -0.0710 0.6051 0.9879
5.500 0.9662 0.01304 0.00699 -0.0717 0.5939 0.9902
5.750 0.9949 0.01305 0.00702 -0.0721 0.5789 0.9929
6.000 1.0212 0.01311 0.00703 -0.0720 0.5592 0.9967
6.250 1.0424 0.01330 0.00719 -0.0710 0.5389 1.0000
6.500 1.0516 0.01352 0.00736 -0.0676 0.5195 1.0000
6.750 1.0593 0.01378 0.00756 -0.0640 0.5012 1.0000
7.000 1.0663 0.01410 0.00784 -0.0603 0.4809 1.0000
7.250 1.0751 0.01449 0.00820 -0.0571 0.4599 1.0000
7.500 1.0855 0.01492 0.00860 -0.0544 0.4392 1.0000
7.750 1.0945 0.01541 0.00905 -0.0515 0.4193 1.0000
8.000 1.1021 0.01595 0.00956 -0.0484 0.4003 1.0000
8.250 1.1083 0.01663 0.01020 -0.0453 0.3778 1.0000
8.500 1.1090 0.01762 0.01107 -0.0419 0.3474 1.0000
8.750 1.1064 0.01901 0.01227 -0.0386 0.3095 1.0000
9.000 1.1006 0.02076 0.01373 -0.0354 0.2639 1.0000
9.250 1.0946 0.02263 0.01529 -0.0323 0.2173 1.0000
9.500 1.0893 0.02457 0.01694 -0.0294 0.1680 1.0000
9.750 1.0852 0.02655 0.01861 -0.0268 0.1223 1.0000
10.000 1.0825 0.02854 0.02032 -0.0244 0.0800 1.0000
10.250 1.0826 0.03041 0.02200 -0.0224 0.0537 1.0000
10.500 1.0855 0.03214 0.02366 -0.0207 0.0386 1.0000
10.750 1.0902 0.03380 0.02530 -0.0192 0.0240 1.0000
11.000 1.0935 0.03562 0.02710 -0.0176 0.0168 1.0000
11.250 1.0965 0.03752 0.02903 -0.0162 0.0136 1.0000
11.500 1.1025 0.03922 0.03084 -0.0150 0.0119 1.0000
11.750 1.1082 0.04098 0.03271 -0.0140 0.0107 1.0000
12.000 1.1107 0.04311 0.03492 -0.0129 0.0094 1.0000
12.250 1.1120 0.04545 0.03738 -0.0119 0.0090 1.0000
12.500 1.1138 0.04783 0.03991 -0.0111 0.0088 1.0000
12.750 1.1171 0.05013 0.04235 -0.0105 0.0085 1.0000
13.000 1.1191 0.05265 0.04501 -0.0099 0.0080 1.0000
13.250 1.1214 0.05519 0.04767 -0.0094 0.0078 1.0000
13.500 1.1230 0.05787 0.05047 -0.0090 0.0077 1.0000
13.750 1.1254 0.06051 0.05323 -0.0087 0.0075 1.0000
14.000 1.1270 0.06330 0.05614 -0.0085 0.0073 1.0000
14.250 1.1291 0.06609 0.05904 -0.0083 0.0071 1.0000
14.500 1.1314 0.06891 0.06198 -0.0083 0.0069 1.0000
14.750 1.1338 0.07176 0.06495 -0.0083 0.0068 1.0000
15.000 1.1362 0.07467 0.06798 -0.0083 0.0067 1.0000
15.250 1.1382 0.07769 0.07112 -0.0085 0.0066 1.0000
15.500 1.1394 0.08087 0.07444 -0.0088 0.0064 1.0000
15.750 1.1413 0.08402 0.07774 -0.0092 0.0064 1.0000
16.000 1.1411 0.08756 0.08145 -0.0097 0.0063 1.0000
16.250 1.1410 0.09115 0.08520 -0.0105 0.0063 1.0000
16.500 1.1393 0.09505 0.08926 -0.0114 0.0062 1.0000
16.750 1.1357 0.09935 0.09373 -0.0126 0.0062 1.0000
17.000 1.1317 0.10381 0.09838 -0.0141 0.0062 1.0000
17.250 1.1264 0.10862 0.10338 -0.0159 0.0062 1.0000
17.500 1.1192 0.11387 0.10881 -0.0181 0.0061 1.0000
17.750 1.1106 0.11950 0.11462 -0.0207 0.0061 1.0000
18.000 1.1015 0.12542 0.12074 -0.0237 0.0061 1.0000
18.250 1.0916 0.13165 0.12714 -0.0270 0.0061 1.0000
18.500 1.0791 0.13880 0.13451 -0.0310 0.0061 1.0000
18.750 1.0668 0.14612 0.14202 -0.0354 0.0062 1.0000
19.000 1.0516 0.15451 0.15061 -0.0405 0.0062 1.0000
19.250 1.0325 0.16449 0.16081 -0.0466 0.0064 1.0000
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