UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Reynolds number: 500,000 Max Cl/Cd: 75.92 at α=3.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ua79sf18-il-500000-n5.txt Download as CSV file: xf-ua79sf18-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL
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 -0.1022 0.08894 0.08525 -0.1403 0.7728 0.0030
-12.500 -0.1193 0.08072 0.07707 -0.1437 0.7724 0.0029
-12.250 -0.1496 0.06708 0.06341 -0.1508 0.7720 0.0027
-12.000 -0.1860 0.05795 0.05415 -0.1552 0.7715 0.0027
-11.750 -0.2091 0.05285 0.04894 -0.1566 0.7709 0.0026
-11.500 -0.2293 0.04871 0.04467 -0.1567 0.7702 0.0025
-11.250 -0.2503 0.04478 0.04060 -0.1558 0.7695 0.0025
-11.000 -0.2679 0.04141 0.03706 -0.1543 0.7688 0.0025
-10.750 -0.2861 0.03805 0.03349 -0.1520 0.7680 0.0025
-10.500 -0.2969 0.03545 0.03070 -0.1496 0.7672 0.0026
-10.250 -0.3028 0.03327 0.02833 -0.1471 0.7663 0.0028
-10.000 -0.3071 0.03095 0.02577 -0.1445 0.7655 0.0026
-9.750 -0.3066 0.02897 0.02357 -0.1419 0.7647 0.0027
-9.500 -0.3009 0.02734 0.02173 -0.1398 0.7640 0.0027
-9.250 -0.2916 0.02597 0.02018 -0.1380 0.7633 0.0029
-9.000 -0.2791 0.02459 0.01861 -0.1364 0.7628 0.0031
-8.750 -0.2631 0.02322 0.01705 -0.1353 0.7624 0.0030
-8.500 -0.2457 0.02223 0.01592 -0.1343 0.7619 0.0033
-8.250 -0.2271 0.02137 0.01493 -0.1334 0.7615 0.0034
-8.000 -0.2078 0.02055 0.01397 -0.1325 0.7611 0.0035
-7.750 -0.1887 0.01969 0.01299 -0.1316 0.7606 0.0036
-7.500 -0.1713 0.01960 0.01285 -0.1305 0.7601 0.0038
-7.250 -0.1535 0.01868 0.01183 -0.1293 0.7595 0.0041
-7.000 -0.1447 0.01772 0.01080 -0.1266 0.7587 0.0045
-6.750 -0.1349 0.01720 0.01023 -0.1240 0.7579 0.0046
-6.500 -0.1222 0.01672 0.00971 -0.1219 0.7572 0.0047
-6.250 -0.1080 0.01628 0.00922 -0.1200 0.7564 0.0048
-6.000 -0.0920 0.01590 0.00878 -0.1184 0.7557 0.0048
-5.750 -0.0751 0.01554 0.00836 -0.1169 0.7549 0.0049
-5.500 -0.0565 0.01523 0.00800 -0.1157 0.7541 0.0051
-5.250 -0.0368 0.01495 0.00766 -0.1146 0.7534 0.0053
-5.000 -0.0158 0.01472 0.00738 -0.1138 0.7527 0.0056
-4.750 0.0062 0.01451 0.00711 -0.1132 0.7520 0.0060
-4.500 0.0287 0.01429 0.00685 -0.1126 0.7513 0.0071
-4.250 0.0518 0.01410 0.00664 -0.1121 0.7507 0.0102
-4.000 0.0712 0.01366 0.00636 -0.1112 0.7500 0.0516
-3.750 0.0922 0.01330 0.00616 -0.1106 0.7495 0.0984
-3.500 0.1025 0.01215 0.00575 -0.1087 0.7488 0.2866
-3.250 0.1088 0.01092 0.00579 -0.1058 0.7482 0.6209
-3.000 0.1374 0.01119 0.00596 -0.1062 0.7478 0.6428
-2.750 0.1659 0.01135 0.00607 -0.1065 0.7474 0.6514
-2.500 0.1944 0.01152 0.00615 -0.1069 0.7469 0.6600
-2.250 0.2197 0.01168 0.00634 -0.1067 0.7461 0.6653
-2.000 0.2432 0.01187 0.00653 -0.1063 0.7448 0.6697
-1.750 0.2675 0.01205 0.00664 -0.1060 0.7435 0.6731
-1.500 0.2925 0.01215 0.00674 -0.1059 0.7423 0.6753
-1.250 0.3183 0.01223 0.00682 -0.1059 0.7411 0.6775
-1.000 0.3449 0.01228 0.00686 -0.1060 0.7400 0.6798
-0.750 0.3725 0.01230 0.00684 -0.1063 0.7389 0.6818
-0.500 0.4008 0.01228 0.00680 -0.1069 0.7380 0.6828
-0.250 0.4294 0.01227 0.00675 -0.1074 0.7373 0.6834
0.000 0.4583 0.01225 0.00670 -0.1080 0.7366 0.6841
0.250 0.4875 0.01223 0.00665 -0.1087 0.7359 0.6847
0.500 0.5175 0.01217 0.00657 -0.1096 0.7353 0.6851
0.750 0.5478 0.01212 0.00649 -0.1105 0.7347 0.6856
1.000 0.5640 0.01241 0.00682 -0.1087 0.7318 0.6863
1.250 0.5837 0.01260 0.00704 -0.1077 0.7293 0.6869
1.500 0.6092 0.01261 0.00705 -0.1076 0.7276 0.6874
2.000 0.6676 0.01238 0.00683 -0.1089 0.7250 0.6882
2.250 0.6984 0.01223 0.00668 -0.1099 0.7239 0.6886
2.500 0.7303 0.01203 0.00650 -0.1110 0.7229 0.6890
2.750 0.7637 0.01182 0.00629 -0.1124 0.7219 0.6891
3.000 0.7671 0.01219 0.00676 -0.1082 0.7164 0.6894
3.250 0.7933 0.01203 0.00663 -0.1081 0.7137 0.6898
3.500 0.8397 0.01106 0.00560 -0.1117 0.7088 0.6900
3.750 0.8277 0.01104 0.00562 -0.1038 0.6909 0.6903
4.000 0.8077 0.01184 0.00649 -0.0952 0.6778 0.6906
4.500 0.8353 0.01163 0.00575 -0.0900 0.5853 0.6910
4.750 0.8115 0.01326 0.00713 -0.0819 0.5481 0.6913
5.000 0.7972 0.01472 0.00840 -0.0756 0.5102 0.6916
5.250 0.7950 0.01582 0.00938 -0.0714 0.4830 0.6918
5.500 0.7724 0.01776 0.01101 -0.0643 0.4305 0.6921
5.750 0.7714 0.01893 0.01201 -0.0606 0.3962 0.6923
6.000 0.7669 0.02030 0.01316 -0.0565 0.3521 0.6925
6.250 0.7617 0.02180 0.01434 -0.0524 0.2961 0.6928
6.500 0.7302 0.02471 0.01638 -0.0451 0.1449 0.6930
6.750 0.7249 0.02651 0.01770 -0.0415 0.0494 0.6932
7.000 0.7347 0.02755 0.01860 -0.0397 0.0064 0.6934
7.250 0.7531 0.02811 0.01920 -0.0390 0.0054 0.6936
7.500 0.7717 0.02866 0.01978 -0.0384 0.0052 0.6938
7.750 0.7899 0.02925 0.02045 -0.0378 0.0048 0.6941
8.000 0.8076 0.02987 0.02113 -0.0371 0.0046 0.6943
8.250 0.8245 0.03056 0.02187 -0.0363 0.0044 0.6945
8.500 0.8411 0.03127 0.02265 -0.0356 0.0042 0.6948
8.750 0.8570 0.03204 0.02349 -0.0347 0.0039 0.6951
9.000 0.8690 0.03311 0.02468 -0.0334 0.0029 0.6953
9.250 0.8842 0.03396 0.02559 -0.0325 0.0030 0.6956
9.500 0.8920 0.03536 0.02711 -0.0309 0.0026 0.6959
9.750 0.9033 0.03654 0.02835 -0.0296 0.0026 0.6961
10.000 0.9184 0.03746 0.02934 -0.0289 0.0025 0.6964
10.250 0.9277 0.03883 0.03079 -0.0276 0.0025 0.6968
10.500 0.9391 0.04009 0.03211 -0.0265 0.0022 0.6970
10.750 0.9479 0.04157 0.03367 -0.0253 0.0021 0.6973
11.000 0.9553 0.04319 0.03536 -0.0240 0.0021 0.6977
11.250 0.9629 0.04484 0.03708 -0.0228 0.0021 0.6980
11.500 0.9703 0.04654 0.03886 -0.0216 0.0021 0.6983
11.750 0.9758 0.04846 0.04086 -0.0204 0.0020 0.6987
12.000 0.9841 0.05014 0.04262 -0.0194 0.0020 0.6990
12.250 0.9906 0.05205 0.04460 -0.0183 0.0020 0.6994
12.500 0.9990 0.05381 0.04644 -0.0174 0.0020 0.6998
12.750 1.0083 0.05552 0.04826 -0.0166 0.0020 0.7003
13.000 1.0183 0.05719 0.05001 -0.0159 0.0020 0.7008
13.250 1.0295 0.05881 0.05171 -0.0152 0.0020 0.7013
13.750 1.0545 0.06196 0.05507 -0.0140 0.0020 0.7025
14.000 1.0674 0.06363 0.05685 -0.0135 0.0020 0.7030
14.250 1.0791 0.06545 0.05880 -0.0131 0.0021 0.7036
14.500 1.0903 0.06750 0.06101 -0.0126 0.0021 0.7041
14.750 1.0986 0.06983 0.06350 -0.0121 0.0021 0.7048
15.000 1.1040 0.07242 0.06625 -0.0118 0.0022 0.7054
15.250 1.1071 0.07559 0.06963 -0.0113 0.0022 0.7060
15.500 1.1068 0.07907 0.07331 -0.0109 0.0023 0.7067
15.750 1.1038 0.08279 0.07722 -0.0108 0.0023 0.7075
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