UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Reynolds number: 200,000 Max Cl/Cd: 34.97 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ua79sf18-il-200000-n5.txt Download as CSV file: xf-ua79sf18-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.000 -0.0900 0.10165 0.09695 -0.1359 0.8056 0.0082
-12.750 -0.0917 0.09769 0.09302 -0.1376 0.8051 0.0077
-12.500 -0.0983 0.09203 0.08741 -0.1399 0.8045 0.0077
-12.250 -0.1027 0.08739 0.08280 -0.1420 0.8040 0.0070
-12.000 -0.1220 0.07688 0.07232 -0.1471 0.8035 0.0073
-11.750 -0.1424 0.06939 0.06477 -0.1515 0.8028 0.0069
-11.500 -0.1618 0.06407 0.05937 -0.1540 0.8022 0.0065
-11.250 -0.1830 0.05947 0.05464 -0.1552 0.8015 0.0065
-11.000 -0.2022 0.05567 0.05072 -0.1553 0.8008 0.0065
-10.750 -0.2221 0.05211 0.04699 -0.1545 0.8001 0.0065
-10.500 -0.2383 0.04914 0.04385 -0.1530 0.7994 0.0066
-10.250 -0.2503 0.04663 0.04112 -0.1511 0.7987 0.0074
-10.000 -0.2633 0.04406 0.03838 -0.1487 0.7979 0.0064
-9.750 -0.2735 0.04196 0.03610 -0.1457 0.7964 0.0067
-9.500 -0.2798 0.04020 0.03416 -0.1427 0.7952 0.0068
-9.250 -0.2836 0.03893 0.03266 -0.1394 0.7936 0.0077
-9.000 -0.2869 0.03763 0.03112 -0.1357 0.7919 0.0080
-8.750 -0.2844 0.03601 0.02927 -0.1327 0.7903 0.0079
-8.500 -0.2764 0.03450 0.02746 -0.1304 0.7891 0.0082
-8.250 -0.2638 0.03295 0.02566 -0.1286 0.7883 0.0082
-8.000 -0.2468 0.03143 0.02387 -0.1274 0.7876 0.0082
-7.750 -0.2266 0.03012 0.02237 -0.1266 0.7870 0.0083
-7.500 -0.2046 0.02894 0.02103 -0.1261 0.7864 0.0083
-7.250 -0.1822 0.02785 0.01981 -0.1255 0.7859 0.0084
-7.000 -0.1638 0.02704 0.01889 -0.1243 0.7853 0.0085
-6.750 -0.1621 0.02701 0.01886 -0.1206 0.7830 0.0086
-6.500 -0.1597 0.02690 0.01872 -0.1169 0.7807 0.0086
-6.250 -0.1570 0.02660 0.01839 -0.1132 0.7786 0.0088
-6.000 -0.1514 0.02616 0.01787 -0.1099 0.7767 0.0090
-5.750 -0.1433 0.02568 0.01728 -0.1070 0.7753 0.0094
-5.500 -0.1312 0.02528 0.01679 -0.1047 0.7743 0.0099
-5.250 -0.1163 0.02490 0.01630 -0.1029 0.7734 0.0109
-5.000 -0.1373 0.02585 0.01728 -0.0951 0.7681 0.0110
-4.750 -0.1376 0.02604 0.01741 -0.0907 0.7648 0.0118
-4.500 -0.1245 0.02585 0.01713 -0.0885 0.7631 0.0142
-4.250 -0.1083 0.02546 0.01677 -0.0869 0.7619 0.0261
-3.750 -0.1326 0.02628 0.01774 -0.0745 0.7520 0.0589
-3.500 -0.1241 0.02517 0.01737 -0.0725 0.7502 0.2096
-3.250 -0.1136 0.02368 0.01692 -0.0710 0.7490 0.4387
-3.000 -0.0951 0.02406 0.01792 -0.0688 0.7480 0.6439
-2.750 -0.1029 0.02514 0.01898 -0.0630 0.7406 0.6648
-2.500 -0.0819 0.02555 0.01933 -0.0615 0.7385 0.6864
-2.250 -0.0586 0.02587 0.01960 -0.0605 0.7371 0.7017
-2.000 -0.0328 0.02608 0.01978 -0.0598 0.7361 0.7111
-1.750 -0.0045 0.02613 0.01972 -0.0601 0.7353 0.7170
-1.500 -0.0105 0.02712 0.02070 -0.0553 0.7286 0.7209
-1.250 0.0125 0.02727 0.02074 -0.0550 0.7265 0.7249
-1.000 0.0395 0.02732 0.02065 -0.0554 0.7250 0.7280
-0.750 0.0672 0.02734 0.02060 -0.0557 0.7239 0.7296
-0.500 0.0961 0.02734 0.02049 -0.0563 0.7231 0.7307
-0.250 0.0991 0.02806 0.02118 -0.0532 0.7169 0.7320
0.000 0.1210 0.02824 0.02130 -0.0528 0.7141 0.7332
0.250 0.1477 0.02829 0.02128 -0.0531 0.7124 0.7342
0.500 0.1766 0.02828 0.02120 -0.0538 0.7112 0.7351
0.750 0.2069 0.02823 0.02107 -0.0546 0.7103 0.7358
1.000 0.2378 0.02816 0.02095 -0.0555 0.7094 0.7367
1.500 0.2647 0.02896 0.02168 -0.0524 0.6986 0.7389
1.750 0.2960 0.02879 0.02146 -0.0534 0.6973 0.7403
2.000 0.3278 0.02859 0.02124 -0.0543 0.6962 0.7414
2.250 0.3596 0.02841 0.02105 -0.0553 0.6954 0.7420
2.500 0.3564 0.02938 0.02203 -0.0514 0.6852 0.7426
2.750 0.3861 0.02927 0.02192 -0.0521 0.6838 0.7430
3.000 0.4170 0.02912 0.02176 -0.0530 0.6827 0.7433
3.500 0.4485 0.02986 0.02254 -0.0507 0.6715 0.7443
3.750 0.4795 0.02964 0.02233 -0.0515 0.6702 0.7448
4.250 0.5194 0.02989 0.02263 -0.0501 0.6591 0.7463
4.500 0.5514 0.02952 0.02232 -0.0510 0.6576 0.7468
5.000 0.5919 0.02987 0.02276 -0.0498 0.6469 0.7479
5.250 0.6235 0.02945 0.02238 -0.0506 0.6450 0.7484
5.500 0.6563 0.02891 0.02192 -0.0515 0.6435 0.7490
6.500 0.7348 0.02810 0.02118 -0.0473 0.5789 0.7518
6.750 0.7785 0.02672 0.01978 -0.0492 0.5656 0.7525
7.000 0.8314 0.02480 0.01777 -0.0521 0.5425 0.7532
7.250 0.8511 0.02434 0.01653 -0.0501 0.4339 0.7540
7.500 0.8462 0.02584 0.01768 -0.0463 0.3751 0.7549
7.750 0.8310 0.02803 0.01938 -0.0414 0.2997 0.7558
8.000 0.8222 0.03009 0.02100 -0.0376 0.2269 0.7568
8.250 0.7890 0.03391 0.02369 -0.0315 0.0542 0.7578
8.500 0.7953 0.03537 0.02497 -0.0298 0.0112 0.7589
8.750 0.8105 0.03623 0.02588 -0.0289 0.0087 0.7601
9.000 0.8263 0.03706 0.02680 -0.0282 0.0079 0.7615
9.250 0.8419 0.03793 0.02778 -0.0275 0.0074 0.7630
9.500 0.8570 0.03886 0.02882 -0.0267 0.0071 0.7646
9.750 0.8718 0.03984 0.02991 -0.0260 0.0070 0.7664
10.000 0.8856 0.04091 0.03116 -0.0251 0.0069 0.7684
10.250 0.8986 0.04206 0.03245 -0.0243 0.0068 0.7708
10.500 0.9107 0.04333 0.03387 -0.0234 0.0066 0.7737
10.750 0.9228 0.04465 0.03532 -0.0226 0.0064 0.7769
11.000 0.9333 0.04612 0.03693 -0.0217 0.0059 0.7802
11.250 0.9432 0.04764 0.03861 -0.0208 0.0055 0.7829
11.500 0.9522 0.04926 0.04040 -0.0199 0.0054 0.7861
11.750 0.9580 0.05123 0.04253 -0.0188 0.0049 0.7898
12.000 0.9659 0.05300 0.04446 -0.0179 0.0050 0.7951
12.250 0.9692 0.05531 0.04693 -0.0168 0.0047 0.8020
12.500 0.9739 0.05755 0.04928 -0.0160 0.0047 0.8126
12.750 0.9789 0.05977 0.05163 -0.0152 0.0047 0.8212
13.000 0.9839 0.06199 0.05404 -0.0145 0.0047 0.8309
13.250 0.9881 0.06431 0.05651 -0.0137 0.0046 0.8421
13.500 0.9936 0.06646 0.05882 -0.0129 0.0046 0.8593
13.750 1.0007 0.06853 0.06106 -0.0123 0.0045 0.8907
14.000 1.0107 0.07043 0.06314 -0.0124 0.0045 0.9503
14.250 1.0180 0.07221 0.06502 -0.0115 0.0045 1.0000
14.500 1.0286 0.07409 0.06700 -0.0111 0.0045 1.0000
14.750 1.0395 0.07600 0.06902 -0.0107 0.0045 1.0000
15.000 1.0498 0.07801 0.07117 -0.0105 0.0046 1.0000
15.250 1.0599 0.08016 0.07347 -0.0101 0.0046 1.0000
15.500 1.0680 0.08257 0.07604 -0.0098 0.0047 1.0000
15.750 1.0738 0.08529 0.07894 -0.0097 0.0047 1.0000
16.000 1.0775 0.08835 0.08221 -0.0097 0.0048 1.0000
16.250 1.0786 0.09176 0.08582 -0.0099 0.0048 1.0000
16.500 1.0772 0.09553 0.08982 -0.0102 0.0049 1.0000
16.750 1.0742 0.09951 0.09400 -0.0108 0.0050 1.0000
17.000 1.0684 0.10402 0.09873 -0.0117 0.0051 1.0000
17.250 1.0620 0.10862 0.10358 -0.0130 0.0051 1.0000
17.500 1.0532 0.11374 0.10891 -0.0146 0.0051 1.0000
17.750 1.0430 0.11924 0.11463 -0.0166 0.0052 1.0000
18.000 1.0318 0.12506 0.12065 -0.0190 0.0053 1.0000
18.250 1.0204 0.13110 0.12688 -0.0218 0.0053 1.0000
18.500 1.0073 0.13767 0.13364 -0.0252 0.0054 1.0000
18.750 0.9954 0.14427 0.14041 -0.0288 0.0054 1.0000
19.000 0.9820 0.15148 0.14779 -0.0330 0.0055 1.0000
19.250 0.9695 0.15886 0.15532 -0.0375 0.0055 1.0000
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