TSAGI 12% AIRFOIL (tsagi12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: TSAGI 12% AIRFOIL (tsagi12-il) Reynolds number: 1,000,000 Max Cl/Cd: 86.5 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tsagi12-il-1000000-n5.txt Download as CSV file: xf-tsagi12-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: TSAGI 12% 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
------ -------- --------- --------- -------- -------- --------
-16.250 -0.7589 0.12417 0.12222 -0.0093 1.0000 0.0049
-16.000 -0.8092 0.10995 0.10794 -0.0167 1.0000 0.0048
-15.750 -1.0820 0.05065 0.04798 -0.0549 1.0000 0.0041
-15.500 -1.1217 0.04226 0.03931 -0.0595 1.0000 0.0040
-15.250 -1.1427 0.03794 0.03479 -0.0594 1.0000 0.0039
-15.000 -1.1396 0.03624 0.03302 -0.0585 1.0000 0.0040
-14.750 -1.1471 0.03383 0.03046 -0.0566 1.0000 0.0041
-14.500 -1.1510 0.03190 0.02840 -0.0542 1.0000 0.0041
-14.250 -1.1522 0.03026 0.02663 -0.0516 1.0000 0.0042
-14.000 -1.1498 0.02895 0.02520 -0.0490 1.0000 0.0042
-13.750 -1.1484 0.02761 0.02373 -0.0459 1.0000 0.0042
-13.500 -1.1409 0.02669 0.02272 -0.0433 1.0000 0.0044
-13.250 -1.1376 0.02560 0.02150 -0.0399 1.0000 0.0044
-13.000 -1.1309 0.02475 0.02056 -0.0367 1.0000 0.0046
-12.750 -1.1248 0.02392 0.01963 -0.0333 1.0000 0.0046
-12.500 -1.1168 0.02300 0.01861 -0.0303 1.0000 0.0047
-12.250 -1.1052 0.02222 0.01772 -0.0278 1.0000 0.0048
-12.000 -1.0938 0.02139 0.01678 -0.0252 1.0000 0.0049
-11.750 -1.0803 0.02070 0.01601 -0.0229 1.0000 0.0050
-11.500 -1.0647 0.02018 0.01541 -0.0208 1.0000 0.0050
-11.250 -1.0530 0.01935 0.01447 -0.0181 1.0000 0.0051
-11.000 -1.0403 0.01859 0.01362 -0.0155 1.0000 0.0054
-10.500 -0.9948 0.01724 0.01215 -0.0144 0.9968 0.0059
-10.250 -0.9694 0.01663 0.01147 -0.0144 0.9911 0.0061
-10.000 -0.9413 0.01603 0.01079 -0.0148 0.9858 0.0064
-9.750 -0.9130 0.01547 0.01017 -0.0153 0.9792 0.0066
-9.500 -0.8803 0.01495 0.00958 -0.0167 0.9734 0.0070
-9.250 -0.8458 0.01443 0.00899 -0.0185 0.9665 0.0072
-9.000 -0.8089 0.01373 0.00823 -0.0209 0.9584 0.0080
-8.750 -0.7691 0.01316 0.00760 -0.0239 0.9462 0.0087
-8.500 -0.7317 0.01270 0.00706 -0.0262 0.9261 0.0095
-8.250 -0.7022 0.01238 0.00660 -0.0267 0.8988 0.0099
-8.000 -0.6790 0.01208 0.00618 -0.0258 0.8720 0.0107
-7.750 -0.6574 0.01182 0.00582 -0.0246 0.8473 0.0119
-7.500 -0.6358 0.01161 0.00550 -0.0233 0.8238 0.0131
-7.250 -0.6136 0.01141 0.00520 -0.0222 0.8031 0.0143
-7.000 -0.5913 0.01119 0.00493 -0.0211 0.7853 0.0165
-6.750 -0.5683 0.01101 0.00467 -0.0201 0.7681 0.0185
-6.500 -0.5449 0.01083 0.00441 -0.0192 0.7517 0.0201
-6.250 -0.5215 0.01064 0.00418 -0.0183 0.7371 0.0222
-6.000 -0.4973 0.01047 0.00396 -0.0176 0.7251 0.0243
-5.750 -0.4726 0.01035 0.00378 -0.0169 0.7130 0.0258
-5.500 -0.4480 0.01021 0.00357 -0.0162 0.7023 0.0270
-5.250 -0.4240 0.01002 0.00332 -0.0155 0.6923 0.0293
-5.000 -0.3994 0.00985 0.00312 -0.0148 0.6823 0.0313
-4.750 -0.3746 0.00971 0.00294 -0.0142 0.6726 0.0331
-4.500 -0.3498 0.00959 0.00276 -0.0135 0.6630 0.0345
-4.250 -0.3248 0.00943 0.00259 -0.0129 0.6548 0.0393
-4.000 -0.3002 0.00928 0.00244 -0.0123 0.6471 0.0462
-3.750 -0.2752 0.00912 0.00231 -0.0117 0.6389 0.0565
-3.500 -0.2501 0.00902 0.00220 -0.0111 0.6310 0.0645
-3.250 -0.2242 0.00895 0.00210 -0.0107 0.6233 0.0674
-3.000 -0.1987 0.00886 0.00198 -0.0102 0.6164 0.0717
-2.750 -0.1731 0.00876 0.00187 -0.0097 0.6095 0.0765
-2.500 -0.1475 0.00870 0.00178 -0.0093 0.6021 0.0800
-2.250 -0.1214 0.00863 0.00169 -0.0089 0.5940 0.0830
-2.000 -0.0959 0.00856 0.00160 -0.0084 0.5865 0.0883
-1.750 -0.0707 0.00843 0.00151 -0.0079 0.5791 0.1027
-1.500 -0.0467 0.00826 0.00144 -0.0071 0.5715 0.1397
-1.250 -0.0217 0.00813 0.00137 -0.0066 0.5622 0.1657
-1.000 0.0032 0.00803 0.00132 -0.0060 0.5533 0.1885
-0.750 0.0272 0.00789 0.00127 -0.0052 0.5431 0.2268
-0.500 0.0485 0.00756 0.00120 -0.0040 0.5328 0.3124
-0.250 0.0687 0.00723 0.00114 -0.0025 0.5215 0.4070
0.000 0.0895 0.00698 0.00110 -0.0012 0.5103 0.4847
0.250 0.1073 0.00664 0.00104 0.0009 0.4988 0.5809
0.500 0.1208 0.00624 0.00100 0.0040 0.4877 0.6952
0.750 0.1348 0.00595 0.00100 0.0071 0.4768 0.7817
1.000 0.1558 0.00582 0.00106 0.0087 0.4665 0.8485
1.250 0.1862 0.00583 0.00114 0.0082 0.4558 0.8854
1.500 0.2241 0.00591 0.00125 0.0060 0.4459 0.9094
1.750 0.2712 0.00609 0.00142 0.0017 0.4360 0.9278
2.000 0.3114 0.00628 0.00158 -0.0011 0.4274 0.9398
2.250 0.3435 0.00641 0.00168 -0.0020 0.4199 0.9431
2.500 0.3707 0.00651 0.00176 -0.0019 0.4129 0.9468
2.750 0.3968 0.00664 0.00187 -0.0015 0.4067 0.9516
3.000 0.4312 0.00678 0.00199 -0.0031 0.3994 0.9531
3.250 0.4623 0.00691 0.00209 -0.0039 0.3926 0.9543
3.500 0.4926 0.00703 0.00219 -0.0045 0.3833 0.9556
3.750 0.5221 0.00717 0.00230 -0.0050 0.3722 0.9575
4.000 0.5479 0.00731 0.00241 -0.0046 0.3641 0.9608
4.250 0.5716 0.00740 0.00251 -0.0037 0.3589 0.9640
4.500 0.6027 0.00753 0.00262 -0.0046 0.3503 0.9647
4.750 0.6337 0.00764 0.00274 -0.0055 0.3433 0.9654
5.000 0.6639 0.00780 0.00287 -0.0062 0.3310 0.9662
5.250 0.6929 0.00801 0.00302 -0.0067 0.3101 0.9673
5.500 0.7199 0.00833 0.00321 -0.0068 0.2792 0.9687
5.750 0.7431 0.00882 0.00349 -0.0063 0.2348 0.9709
6.000 0.7574 0.00940 0.00384 -0.0039 0.1879 0.9753
6.250 0.7841 0.00996 0.00420 -0.0042 0.1476 0.9761
6.500 0.8087 0.01066 0.00466 -0.0042 0.0980 0.9772
6.750 0.8347 0.01115 0.00504 -0.0044 0.0743 0.9784
7.000 0.8589 0.01174 0.00548 -0.0042 0.0456 0.9800
7.250 0.8824 0.01225 0.00590 -0.0038 0.0292 0.9821
7.500 0.9014 0.01264 0.00628 -0.0023 0.0218 0.9851
7.750 0.9282 0.01303 0.00665 -0.0026 0.0167 0.9860
8.000 0.9557 0.01341 0.00704 -0.0031 0.0135 0.9867
8.250 0.9831 0.01377 0.00742 -0.0035 0.0121 0.9877
8.500 1.0094 0.01421 0.00786 -0.0038 0.0106 0.9889
8.750 1.0349 0.01463 0.00831 -0.0039 0.0097 0.9902
9.000 1.0597 0.01502 0.00873 -0.0038 0.0089 0.9916
9.250 1.0827 0.01547 0.00922 -0.0034 0.0085 0.9932
9.500 1.1050 0.01597 0.00974 -0.0030 0.0076 0.9946
9.750 1.1298 0.01658 0.01039 -0.0032 0.0070 0.9957
10.000 1.1548 0.01704 0.01090 -0.0034 0.0067 0.9969
10.250 1.1784 0.01755 0.01145 -0.0034 0.0063 0.9981
10.500 1.2009 0.01813 0.01207 -0.0033 0.0061 0.9992
10.750 1.2177 0.01866 0.01265 -0.0020 0.0058 1.0000
11.000 1.2153 0.01911 0.01315 0.0033 0.0057 1.0000
11.250 1.2159 0.01965 0.01374 0.0077 0.0055 1.0000
11.500 1.2170 0.02034 0.01448 0.0116 0.0053 1.0000
11.750 1.2162 0.02128 0.01549 0.0155 0.0050 1.0000
12.000 1.2193 0.02219 0.01645 0.0184 0.0049 1.0000
12.250 1.2238 0.02315 0.01749 0.0209 0.0049 1.0000
12.500 1.2285 0.02423 0.01863 0.0231 0.0047 1.0000
12.750 1.2323 0.02548 0.01996 0.0251 0.0046 1.0000
13.000 1.2415 0.02645 0.02097 0.0265 0.0044 1.0000
13.250 1.2421 0.02818 0.02279 0.0282 0.0043 1.0000
13.500 1.2461 0.02974 0.02442 0.0294 0.0042 1.0000
13.750 1.2497 0.03145 0.02621 0.0305 0.0040 1.0000
14.000 1.2503 0.03351 0.02835 0.0314 0.0040 1.0000
14.250 1.2568 0.03511 0.03000 0.0320 0.0039 1.0000
14.500 1.2593 0.03714 0.03211 0.0325 0.0038 1.0000
14.750 1.2590 0.03955 0.03460 0.0330 0.0038 1.0000
15.000 1.2581 0.04207 0.03720 0.0332 0.0037 1.0000
15.250 1.2548 0.04494 0.04015 0.0334 0.0036 1.0000
15.500 1.2514 0.04791 0.04319 0.0333 0.0035 1.0000
15.750 1.2449 0.05135 0.04674 0.0330 0.0034 1.0000
16.000 1.2437 0.05430 0.04979 0.0326 0.0036 1.0000
16.250 1.2319 0.05869 0.05427 0.0318 0.0033 1.0000
16.500 1.2249 0.06260 0.05829 0.0309 0.0033 1.0000
16.750 1.2190 0.06648 0.06225 0.0299 0.0033 1.0000
17.000 1.2118 0.07062 0.06650 0.0287 0.0033 1.0000
17.250 1.2037 0.07496 0.07093 0.0274 0.0033 1.0000
17.500 1.2007 0.07868 0.07474 0.0262 0.0033 1.0000
17.750 1.1919 0.08330 0.07946 0.0247 0.0032 1.0000
18.000 1.1846 0.08775 0.08402 0.0232 0.0032 1.0000
18.250 1.1714 0.09321 0.08958 0.0212 0.0032 1.0000
18.500 1.1643 0.09783 0.09430 0.0194 0.0032 1.0000
18.750 1.1514 0.10345 0.10003 0.0172 0.0031 1.0000
19.000 1.1409 0.10878 0.10545 0.0150 0.0031 1.0000
19.250 1.1290 0.11448 0.11125 0.0126 0.0031 1.0000
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