UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Reynolds number: 100,000 Max Cl/Cd: 23.11 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ua79sf18-il-100000-n5.txt Download as CSV file: xf-ua79sf18-il-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.250 -0.0705 0.11386 0.10795 -0.1383 0.8506 0.0183
-13.000 -0.0707 0.10971 0.10383 -0.1400 0.8500 0.0177
-12.750 -0.0727 0.10526 0.09943 -0.1419 0.8494 0.0172
-12.500 -0.0781 0.09994 0.09418 -0.1440 0.8488 0.0166
-12.250 -0.0904 0.09228 0.08662 -0.1474 0.8482 0.0156
-12.000 -0.1139 0.08144 0.07574 -0.1533 0.8474 0.0147
-11.750 -0.1277 0.07653 0.07070 -0.1563 0.8466 0.0144
-11.500 -0.1421 0.07242 0.06655 -0.1581 0.8457 0.0143
-11.250 -0.1589 0.06867 0.06272 -0.1591 0.8448 0.0142
-11.000 -0.1750 0.06548 0.05945 -0.1592 0.8436 0.0141
-10.750 -0.1941 0.06245 0.05628 -0.1586 0.8420 0.0141
-10.500 -0.2107 0.05990 0.05361 -0.1573 0.8408 0.0140
-10.250 -0.2270 0.05764 0.05120 -0.1553 0.8396 0.0140
-10.000 -0.2400 0.05587 0.04928 -0.1530 0.8385 0.0139
-9.750 -0.2561 0.05414 0.04737 -0.1496 0.8367 0.0139
-9.500 -0.2774 0.05371 0.04688 -0.1442 0.8331 0.0139
-9.250 -0.2998 0.05324 0.04631 -0.1382 0.8300 0.0138
-9.000 -0.3175 0.05249 0.04541 -0.1325 0.8276 0.0138
-8.750 -0.3280 0.05141 0.04413 -0.1279 0.8258 0.0138
-8.500 -0.3343 0.04988 0.04234 -0.1238 0.8245 0.0138
-8.250 -0.3746 0.05145 0.04401 -0.1133 0.8198 0.0138
-8.000 -0.3948 0.05111 0.04355 -0.1062 0.8162 0.0138
-7.750 -0.3980 0.04978 0.04197 -0.1019 0.8139 0.0138
-7.500 -0.3929 0.04813 0.04003 -0.0990 0.8124 0.0138
-7.250 -0.3804 0.04635 0.03792 -0.0970 0.8114 0.0139
-7.000 -0.4261 0.04755 0.03921 -0.0853 0.8058 0.0138
-6.500 -0.4086 0.04504 0.03617 -0.0798 0.8020 0.0140
-6.250 -0.3885 0.04369 0.03459 -0.0787 0.8006 0.0142
-6.000 -0.3661 0.04245 0.03315 -0.0779 0.7995 0.0144
-5.500 -0.3587 0.04104 0.03163 -0.0708 0.7951 0.0151
-5.250 -0.3560 0.04049 0.03103 -0.0672 0.7924 0.0158
-5.000 -0.3437 0.03987 0.03034 -0.0651 0.7901 0.0165
-4.750 -0.3279 0.03928 0.02966 -0.0635 0.7884 0.0180
-4.500 -0.3068 0.03884 0.02905 -0.0628 0.7869 0.0218
-4.250 -0.2849 0.03793 0.02804 -0.0622 0.7856 0.0264
-4.000 -0.2906 0.03785 0.02791 -0.0573 0.7799 0.0292
-3.750 -0.2748 0.03733 0.02729 -0.0555 0.7773 0.0375
-3.500 -0.2580 0.03636 0.02670 -0.0542 0.7754 0.0962
-3.250 -0.2600 0.03375 0.02676 -0.0503 0.7737 0.5219
-3.000 -0.2474 0.03484 0.02782 -0.0470 0.7706 0.6620
-2.750 -0.2418 0.03561 0.02854 -0.0426 0.7664 0.6908
-2.500 -0.2296 0.03656 0.02950 -0.0381 0.7638 0.7211
-2.250 -0.2128 0.03732 0.03019 -0.0345 0.7617 0.7448
-2.000 -0.1891 0.03778 0.03043 -0.0328 0.7602 0.7582
-1.750 -0.1856 0.03811 0.03066 -0.0294 0.7549 0.7677
-1.500 -0.1680 0.03838 0.03080 -0.0277 0.7517 0.7732
-1.250 -0.1412 0.03845 0.03067 -0.0282 0.7495 0.7779
-1.000 -0.1112 0.03851 0.03054 -0.0292 0.7478 0.7807
-0.750 -0.1007 0.03878 0.03073 -0.0271 0.7431 0.7833
-0.500 -0.0810 0.03893 0.03076 -0.0266 0.7392 0.7858
-0.250 -0.0531 0.03902 0.03070 -0.0273 0.7368 0.7881
0.000 -0.0218 0.03910 0.03063 -0.0287 0.7351 0.7899
0.250 -0.0118 0.03939 0.03085 -0.0269 0.7291 0.7919
0.500 0.0125 0.03953 0.03086 -0.0271 0.7257 0.7934
0.750 0.0423 0.03962 0.03085 -0.0280 0.7236 0.7945
1.000 0.0751 0.03968 0.03080 -0.0294 0.7220 0.7957
1.500 0.1113 0.04010 0.03109 -0.0282 0.7113 0.7991
1.750 0.1441 0.04014 0.03105 -0.0296 0.7095 0.8004
2.000 0.1527 0.04059 0.03147 -0.0279 0.7016 0.8026
2.250 0.1801 0.04070 0.03155 -0.0284 0.6985 0.8043
2.500 0.2111 0.04074 0.03155 -0.0295 0.6965 0.8056
3.000 0.2478 0.04137 0.03215 -0.0285 0.6855 0.8084
3.250 0.2788 0.04139 0.03216 -0.0296 0.6833 0.8093
3.500 0.2905 0.04191 0.03269 -0.0284 0.6756 0.8106
3.750 0.3183 0.04199 0.03276 -0.0291 0.6722 0.8117
4.000 0.3505 0.04193 0.03270 -0.0304 0.6700 0.8130
4.250 0.3628 0.04242 0.03321 -0.0292 0.6613 0.8148
4.500 0.3941 0.04227 0.03307 -0.0302 0.6583 0.8163
5.000 0.4382 0.04260 0.03348 -0.0300 0.6465 0.8188
5.250 0.4708 0.04237 0.03333 -0.0311 0.6441 0.8201
5.500 0.4828 0.04302 0.03404 -0.0299 0.6348 0.8217
5.750 0.5136 0.04284 0.03391 -0.0308 0.6315 0.8234
6.000 0.5482 0.04243 0.03357 -0.0321 0.6294 0.8251
6.250 0.5582 0.04318 0.03439 -0.0307 0.6183 0.8272
6.500 0.5927 0.04268 0.03402 -0.0319 0.6157 0.8293
6.750 0.6033 0.04339 0.03483 -0.0305 0.6048 0.8313
7.000 0.6361 0.04290 0.03445 -0.0314 0.6021 0.8335
7.500 0.6814 0.04305 0.03484 -0.0311 0.5888 0.8390
7.750 0.6965 0.04366 0.03556 -0.0303 0.5787 0.8423
8.000 0.7354 0.04075 0.03272 -0.0298 0.5617 0.8457
8.750 0.8027 0.03998 0.03234 -0.0279 0.5111 0.8602
9.000 0.8387 0.03811 0.03023 -0.0276 0.4575 0.8669
9.250 0.8662 0.03756 0.02953 -0.0272 0.4186 0.8746
9.500 0.8798 0.03807 0.02971 -0.0257 0.3594 0.8843
9.750 0.8842 0.03944 0.03074 -0.0237 0.3012 0.8968
10.250 0.8714 0.04458 0.03455 -0.0194 0.1025 0.9357
10.750 0.8766 0.04843 0.03780 -0.0166 0.0132 1.0000
11.000 0.8895 0.04989 0.03933 -0.0162 0.0119 1.0000
11.250 0.9024 0.05135 0.04092 -0.0158 0.0114 1.0000
11.500 0.9143 0.05290 0.04262 -0.0154 0.0110 1.0000
11.750 0.9247 0.05462 0.04450 -0.0148 0.0106 1.0000
12.000 0.9351 0.05635 0.04638 -0.0143 0.0104 1.0000
12.250 0.9430 0.05835 0.04856 -0.0137 0.0101 1.0000
12.500 0.9502 0.06045 0.05082 -0.0132 0.0100 1.0000
12.750 0.9563 0.06269 0.05323 -0.0126 0.0098 1.0000
13.000 0.9613 0.06508 0.05579 -0.0122 0.0097 1.0000
13.250 0.9642 0.06779 0.05874 -0.0117 0.0096 1.0000
13.500 0.9666 0.07056 0.06167 -0.0113 0.0095 1.0000
13.750 0.9683 0.07347 0.06475 -0.0110 0.0094 1.0000
14.000 0.9701 0.07641 0.06784 -0.0108 0.0093 1.0000
14.250 0.9726 0.07930 0.07087 -0.0107 0.0092 1.0000
14.500 0.9737 0.08237 0.07406 -0.0106 0.0087 1.0000
14.750 0.9768 0.08521 0.07701 -0.0106 0.0085 1.0000
15.000 0.9835 0.08761 0.07954 -0.0106 0.0086 1.0000
15.250 0.9864 0.09037 0.08235 -0.0104 0.0078 1.0000
15.500 0.9965 0.09228 0.08433 -0.0100 0.0075 1.0000
15.750 1.0097 0.09398 0.08614 -0.0094 0.0073 1.0000
16.000 1.0186 0.09640 0.08870 -0.0094 0.0072 1.0000
16.250 1.0252 0.09913 0.09162 -0.0096 0.0071 1.0000
16.500 1.0297 0.10221 0.09490 -0.0099 0.0071 1.0000
16.750 1.0327 0.10551 0.09839 -0.0105 0.0072 1.0000
17.000 1.0321 0.10936 0.10245 -0.0113 0.0072 1.0000
17.250 1.0303 0.11339 0.10668 -0.0124 0.0072 1.0000
17.500 1.0257 0.11790 0.11141 -0.0139 0.0072 1.0000
18.500 0.9967 0.13849 0.13291 -0.0234 0.0073 1.0000
18.750 0.9891 0.14406 0.13866 -0.0266 0.0074 1.0000
19.000 0.9801 0.15016 0.14493 -0.0302 0.0074 1.0000
19.250 0.9715 0.15643 0.15138 -0.0341 0.0075 1.0000
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