UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Reynolds number: 1,000,000 Max Cl/Cd: 114.11 at α=3° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ua79sf18-il-1000000-n5.txt Download as CSV file: xf-ua79sf18-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.250 -0.2453 0.05951 0.05632 -0.1515 0.7580 0.0014
-13.000 -0.2554 0.05471 0.05145 -0.1544 0.7576 0.0014
-12.750 -0.2814 0.04892 0.04552 -0.1565 0.7570 0.0013
-12.500 -0.3079 0.04398 0.04042 -0.1569 0.7562 0.0013
-12.250 -0.3165 0.04128 0.03763 -0.1566 0.7556 0.0012
-12.000 -0.3417 0.03709 0.03321 -0.1551 0.7547 0.0013
-11.750 -0.3522 0.03445 0.03041 -0.1536 0.7540 0.0013
-11.500 -0.3589 0.03221 0.02802 -0.1519 0.7532 0.0013
-11.250 -0.3642 0.03004 0.02568 -0.1500 0.7526 0.0013
-11.000 -0.3641 0.02833 0.02382 -0.1482 0.7520 0.0013
-10.750 -0.3646 0.02644 0.02173 -0.1460 0.7513 0.0014
-10.500 -0.3565 0.02534 0.02051 -0.1445 0.7508 0.0014
-10.250 -0.3423 0.02491 0.02003 -0.1436 0.7503 0.0015
-10.000 -0.3416 0.02267 0.01754 -0.1410 0.7497 0.0014
-9.750 -0.3291 0.02176 0.01652 -0.1396 0.7492 0.0015
-9.500 -0.3155 0.02091 0.01557 -0.1383 0.7487 0.0015
-9.250 -0.3053 0.01910 0.01352 -0.1365 0.7482 0.0018
-9.000 -0.2917 0.01807 0.01238 -0.1350 0.7476 0.0019
-8.750 -0.2743 0.01750 0.01172 -0.1340 0.7471 0.0018
-8.500 -0.2607 0.01666 0.01082 -0.1324 0.7466 0.0020
-8.250 -0.2441 0.01615 0.01027 -0.1313 0.7463 0.0021
-8.000 -0.2283 0.01561 0.00969 -0.1299 0.7458 0.0022
-7.750 -0.2158 0.01498 0.00899 -0.1278 0.7453 0.0022
-7.500 -0.2000 0.01470 0.00870 -0.1263 0.7447 0.0024
-7.250 -0.1874 0.01424 0.00819 -0.1240 0.7441 0.0024
-7.000 -0.1708 0.01382 0.00772 -0.1225 0.7436 0.0025
-6.750 -0.1539 0.01337 0.00723 -0.1211 0.7431 0.0026
-6.500 -0.1352 0.01299 0.00680 -0.1199 0.7425 0.0026
-6.250 -0.1157 0.01263 0.00640 -0.1189 0.7420 0.0027
-6.000 -0.0936 0.01239 0.00614 -0.1184 0.7415 0.0031
-5.750 -0.0724 0.01207 0.00579 -0.1176 0.7410 0.0032
-5.500 -0.0503 0.01178 0.00546 -0.1170 0.7404 0.0034
-5.250 -0.0281 0.01147 0.00511 -0.1164 0.7398 0.0035
-5.000 -0.0048 0.01120 0.00479 -0.1160 0.7391 0.0035
-4.750 0.0193 0.01097 0.00452 -0.1157 0.7386 0.0036
-4.500 0.0440 0.01077 0.00428 -0.1155 0.7381 0.0037
-4.250 0.0695 0.01060 0.00406 -0.1155 0.7377 0.0038
-4.000 0.0953 0.01044 0.00386 -0.1155 0.7373 0.0047
-3.750 0.1213 0.01029 0.00371 -0.1155 0.7368 0.0079
-3.500 0.1446 0.00994 0.00351 -0.1152 0.7363 0.0461
-3.250 0.1627 0.00921 0.00323 -0.1142 0.7359 0.1695
-3.000 0.1812 0.00844 0.00295 -0.1135 0.7354 0.3114
-2.750 0.1940 0.00721 0.00277 -0.1118 0.7349 0.6169
-2.500 0.2238 0.00737 0.00285 -0.1125 0.7345 0.6318
-2.250 0.2528 0.00745 0.00294 -0.1130 0.7341 0.6379
-2.000 0.2817 0.00758 0.00301 -0.1135 0.7336 0.6447
-1.750 0.3103 0.00762 0.00305 -0.1140 0.7330 0.6484
-1.500 0.3389 0.00766 0.00309 -0.1145 0.7322 0.6512
-1.250 0.3676 0.00769 0.00311 -0.1151 0.7314 0.6535
-1.000 0.3964 0.00772 0.00313 -0.1156 0.7305 0.6556
-0.750 0.4253 0.00777 0.00315 -0.1162 0.7298 0.6576
-0.500 0.4541 0.00781 0.00318 -0.1168 0.7291 0.6590
-0.250 0.4830 0.00782 0.00317 -0.1174 0.7284 0.6601
0.000 0.5118 0.00780 0.00315 -0.1180 0.7275 0.6611
0.250 0.5408 0.00777 0.00312 -0.1186 0.7265 0.6618
0.500 0.5699 0.00773 0.00308 -0.1193 0.7254 0.6623
0.750 0.5991 0.00770 0.00304 -0.1200 0.7244 0.6627
1.000 0.6283 0.00767 0.00301 -0.1206 0.7234 0.6628
1.250 0.6578 0.00765 0.00298 -0.1214 0.7224 0.6630
1.500 0.6859 0.00765 0.00300 -0.1218 0.7211 0.6632
1.750 0.7129 0.00765 0.00303 -0.1221 0.7189 0.6637
2.000 0.7404 0.00762 0.00302 -0.1224 0.7164 0.6641
2.250 0.7684 0.00756 0.00297 -0.1228 0.7135 0.6645
2.500 0.7971 0.00748 0.00290 -0.1233 0.7105 0.6649
2.750 0.8208 0.00734 0.00274 -0.1227 0.6971 0.6653
3.000 0.8353 0.00732 0.00257 -0.1201 0.6519 0.6654
3.250 0.8358 0.00776 0.00279 -0.1148 0.6103 0.6656
3.500 0.8091 0.00848 0.00328 -0.1040 0.5624 0.6658
3.750 0.7846 0.00955 0.00420 -0.0944 0.5282 0.6660
4.000 0.7697 0.01083 0.00536 -0.0875 0.4973 0.6662
4.250 0.7652 0.01200 0.00643 -0.0828 0.4719 0.6663
4.500 0.7314 0.01423 0.00832 -0.0735 0.4087 0.6665
4.750 0.7157 0.01584 0.00964 -0.0672 0.3513 0.6667
5.000 0.6982 0.01758 0.01097 -0.0608 0.2758 0.6669
5.250 0.7118 0.01816 0.01150 -0.0592 0.2584 0.6670
5.500 0.6585 0.02172 0.01394 -0.0481 0.0240 0.6671
5.750 0.6755 0.02226 0.01443 -0.0472 0.0067 0.6672
6.000 0.6946 0.02271 0.01488 -0.0465 0.0052 0.6673
6.250 0.7139 0.02316 0.01533 -0.0459 0.0045 0.6674
6.500 0.7331 0.02362 0.01582 -0.0453 0.0034 0.6675
6.750 0.7524 0.02409 0.01630 -0.0446 0.0033 0.6676
7.000 0.7714 0.02458 0.01683 -0.0440 0.0031 0.6677
7.250 0.7899 0.02510 0.01740 -0.0433 0.0029 0.6678
7.500 0.8074 0.02568 0.01802 -0.0424 0.0027 0.6679
7.750 0.8249 0.02627 0.01864 -0.0417 0.0025 0.6680
8.000 0.8425 0.02686 0.01926 -0.0409 0.0023 0.6682
8.250 0.8595 0.02750 0.01994 -0.0401 0.0021 0.6683
8.500 0.8765 0.02815 0.02061 -0.0393 0.0018 0.6684
8.750 0.8919 0.02891 0.02141 -0.0384 0.0018 0.6685
9.000 0.9069 0.02970 0.02224 -0.0374 0.0015 0.6687
9.250 0.9215 0.03054 0.02312 -0.0364 0.0016 0.6688
9.500 0.9357 0.03141 0.02404 -0.0354 0.0013 0.6689
9.750 0.9496 0.03232 0.02501 -0.0343 0.0014 0.6690
10.000 0.9613 0.03340 0.02613 -0.0331 0.0012 0.6691
10.250 0.9733 0.03449 0.02727 -0.0320 0.0012 0.6693
10.500 0.9680 0.03688 0.02977 -0.0289 0.0010 0.6694
10.750 0.9761 0.03833 0.03128 -0.0276 0.0010 0.6695
11.000 0.9850 0.03976 0.03276 -0.0263 0.0010 0.6697
11.250 0.9943 0.04118 0.03424 -0.0251 0.0010 0.6698
11.500 1.0013 0.04281 0.03592 -0.0238 0.0010 0.6700
11.750 1.0088 0.04445 0.03763 -0.0226 0.0009 0.6701
12.000 1.0169 0.04606 0.03929 -0.0215 0.0009 0.6702
12.250 1.0252 0.04771 0.04101 -0.0204 0.0009 0.6704
12.500 1.0339 0.04933 0.04270 -0.0195 0.0009 0.6705
12.750 1.0437 0.05089 0.04432 -0.0186 0.0009 0.6706
13.000 1.0539 0.05245 0.04594 -0.0178 0.0009 0.6708
13.250 1.0654 0.05397 0.04752 -0.0171 0.0009 0.6710
13.500 1.0778 0.05543 0.04905 -0.0164 0.0009 0.6711
13.750 1.0915 0.05686 0.05055 -0.0159 0.0009 0.6713
14.000 1.1055 0.05833 0.05210 -0.0154 0.0009 0.6715
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