WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 76-100 (fx76100-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.13 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx76100-il-1000000.txt Download as CSV file: xf-fx76100-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 76-100
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.000 -1.1030 0.09848 0.09586 -0.0035 1.0000 0.0092
-16.750 -1.1315 0.08944 0.08670 -0.0084 1.0000 0.0091
-16.500 -1.1691 0.07918 0.07627 -0.0140 1.0000 0.0091
-16.000 -1.1997 0.06581 0.06269 -0.0218 1.0000 0.0091
-15.750 -1.2268 0.05728 0.05395 -0.0271 1.0000 0.0093
-15.500 -1.2283 0.05304 0.04963 -0.0299 1.0000 0.0092
-15.250 -1.2413 0.04734 0.04376 -0.0334 1.0000 0.0092
-15.000 -1.2587 0.04157 0.03781 -0.0365 1.0000 0.0092
-14.750 -1.2846 0.03574 0.03174 -0.0382 1.0000 0.0095
-14.500 -1.2888 0.03298 0.02884 -0.0380 1.0000 0.0095
-14.250 -1.2932 0.03054 0.02630 -0.0370 1.0000 0.0099
-14.000 -1.2908 0.02887 0.02451 -0.0355 1.0000 0.0097
-13.750 -1.2907 0.02719 0.02272 -0.0333 1.0000 0.0101
-13.500 -1.2837 0.02609 0.02155 -0.0313 1.0000 0.0103
-13.250 -1.2749 0.02518 0.02057 -0.0292 1.0000 0.0105
-13.000 -1.2663 0.02431 0.01962 -0.0267 1.0000 0.0107
-12.750 -1.2562 0.02343 0.01866 -0.0244 1.0000 0.0110
-12.500 -1.2411 0.02270 0.01786 -0.0228 1.0000 0.0113
-12.250 -1.2272 0.02186 0.01693 -0.0210 1.0000 0.0116
-12.000 -1.2125 0.02103 0.01601 -0.0193 1.0000 0.0117
-11.750 -1.1926 0.02060 0.01551 -0.0182 1.0000 0.0121
-11.500 -1.1820 0.01938 0.01417 -0.0158 1.0000 0.0126
-11.250 -1.1673 0.01846 0.01318 -0.0139 1.0000 0.0130
-11.000 -1.1475 0.01798 0.01269 -0.0127 1.0000 0.0137
-10.750 -1.1286 0.01740 0.01205 -0.0114 1.0000 0.0143
-10.500 -1.1085 0.01693 0.01153 -0.0101 1.0000 0.0148
-10.250 -1.0875 0.01653 0.01107 -0.0090 1.0000 0.0154
-10.000 -1.0671 0.01609 0.01057 -0.0077 1.0000 0.0158
-9.750 -1.0522 0.01515 0.00957 -0.0056 1.0000 0.0169
-9.500 -1.0320 0.01471 0.00912 -0.0043 1.0000 0.0179
-9.250 -1.0113 0.01433 0.00871 -0.0030 1.0000 0.0188
-9.000 -0.9904 0.01399 0.00833 -0.0017 1.0000 0.0196
-8.750 -0.9690 0.01371 0.00800 -0.0004 1.0000 0.0201
-8.500 -0.9521 0.01303 0.00729 0.0016 1.0000 0.0220
-8.250 -0.9316 0.01271 0.00696 0.0030 1.0000 0.0233
-8.000 -0.9110 0.01243 0.00666 0.0044 1.0000 0.0246
-7.750 -0.8899 0.01222 0.00641 0.0057 1.0000 0.0255
-7.500 -0.8723 0.01168 0.00585 0.0077 1.0000 0.0279
-7.250 -0.8526 0.01138 0.00555 0.0093 1.0000 0.0297
-7.000 -0.8324 0.01114 0.00528 0.0108 1.0000 0.0313
-6.750 -0.8123 0.01089 0.00501 0.0123 1.0000 0.0332
-6.500 -0.7925 0.01054 0.00467 0.0139 1.0000 0.0368
-6.250 -0.7583 0.01030 0.00443 0.0124 0.9985 0.0399
-6.000 -0.7251 0.00994 0.00410 0.0112 0.9968 0.0465
-5.750 -0.6921 0.00966 0.00384 0.0099 0.9950 0.0535
-5.500 -0.6600 0.00932 0.00356 0.0089 0.9928 0.0651
-5.250 -0.6271 0.00896 0.00330 0.0077 0.9909 0.0826
-5.000 -0.5935 0.00860 0.00306 0.0063 0.9893 0.1065
-4.750 -0.5612 0.00825 0.00284 0.0052 0.9863 0.1336
-4.500 -0.5257 0.00796 0.00265 0.0035 0.9835 0.1567
-4.250 -0.4893 0.00768 0.00248 0.0016 0.9816 0.1785
-4.000 -0.4573 0.00745 0.00232 0.0007 0.9784 0.1988
-3.750 -0.4245 0.00724 0.00217 -0.0003 0.9748 0.2172
-3.500 -0.3881 0.00698 0.00202 -0.0022 0.9720 0.2399
-3.250 -0.3543 0.00677 0.00188 -0.0034 0.9668 0.2619
-3.000 -0.3192 0.00652 0.00174 -0.0050 0.9614 0.2912
-2.750 -0.2850 0.00628 0.00162 -0.0064 0.9553 0.3213
-2.500 -0.2514 0.00605 0.00150 -0.0076 0.9464 0.3552
-2.250 -0.2215 0.00581 0.00140 -0.0080 0.9353 0.3944
-2.000 -0.1921 0.00560 0.00130 -0.0083 0.9226 0.4346
-1.750 -0.1646 0.00541 0.00122 -0.0081 0.9086 0.4753
-1.500 -0.1387 0.00523 0.00115 -0.0075 0.8925 0.5165
-1.250 -0.1134 0.00510 0.00109 -0.0068 0.8744 0.5551
-1.000 -0.0894 0.00496 0.00104 -0.0058 0.8542 0.5962
-0.750 -0.0659 0.00488 0.00100 -0.0046 0.8293 0.6317
-0.500 -0.0433 0.00481 0.00096 -0.0032 0.8026 0.6671
-0.250 -0.0218 0.00476 0.00094 -0.0016 0.7712 0.7048
0.000 -0.0001 0.00475 0.00093 0.0000 0.7388 0.7399
0.250 0.0217 0.00476 0.00094 0.0016 0.7060 0.7733
0.500 0.0435 0.00480 0.00096 0.0032 0.6693 0.8035
0.750 0.0659 0.00487 0.00100 0.0046 0.6321 0.8298
1.000 0.0892 0.00497 0.00104 0.0058 0.5937 0.8536
1.250 0.1134 0.00510 0.00109 0.0068 0.5555 0.8742
1.500 0.1387 0.00523 0.00115 0.0075 0.5169 0.8922
1.750 0.1645 0.00542 0.00122 0.0081 0.4727 0.9091
2.000 0.1921 0.00561 0.00131 0.0083 0.4334 0.9230
2.250 0.2216 0.00580 0.00140 0.0080 0.3987 0.9351
2.500 0.2514 0.00604 0.00150 0.0076 0.3554 0.9463
2.750 0.2850 0.00629 0.00161 0.0064 0.3194 0.9552
3.000 0.3194 0.00652 0.00174 0.0050 0.2914 0.9615
3.250 0.3543 0.00676 0.00187 0.0035 0.2630 0.9667
3.500 0.3883 0.00698 0.00202 0.0022 0.2401 0.9720
3.750 0.4247 0.00724 0.00217 0.0003 0.2171 0.9749
4.000 0.4573 0.00745 0.00232 -0.0007 0.1987 0.9784
4.250 0.4894 0.00768 0.00247 -0.0016 0.1795 0.9816
4.500 0.5256 0.00796 0.00265 -0.0035 0.1564 0.9835
4.750 0.5613 0.00824 0.00284 -0.0052 0.1339 0.9863
5.000 0.5936 0.00861 0.00307 -0.0063 0.1054 0.9893
5.250 0.6273 0.00897 0.00331 -0.0077 0.0817 0.9909
5.500 0.6600 0.00934 0.00357 -0.0089 0.0637 0.9929
5.750 0.6920 0.00967 0.00384 -0.0099 0.0528 0.9950
6.000 0.7252 0.00995 0.00411 -0.0112 0.0462 0.9968
6.250 0.7583 0.01031 0.00443 -0.0124 0.0399 0.9986
6.500 0.7926 0.01055 0.00468 -0.0139 0.0367 1.0000
6.750 0.8120 0.01090 0.00501 -0.0123 0.0329 1.0000
7.000 0.8322 0.01114 0.00528 -0.0108 0.0313 1.0000
7.250 0.8524 0.01139 0.00555 -0.0092 0.0297 1.0000
7.500 0.8722 0.01169 0.00585 -0.0077 0.0279 1.0000
7.750 0.8895 0.01225 0.00644 -0.0056 0.0255 1.0000
8.000 0.9105 0.01246 0.00670 -0.0043 0.0247 1.0000
8.250 0.9315 0.01272 0.00697 -0.0029 0.0235 1.0000
8.500 0.9519 0.01305 0.00732 -0.0015 0.0222 1.0000
8.750 0.9699 0.01363 0.00791 0.0003 0.0204 1.0000
9.000 0.9902 0.01401 0.00835 0.0017 0.0197 1.0000
9.250 1.0110 0.01436 0.00874 0.0030 0.0189 1.0000
9.500 1.0321 0.01470 0.00911 0.0043 0.0180 1.0000
9.750 1.0524 0.01513 0.00955 0.0056 0.0171 1.0000
10.000 1.0687 0.01594 0.01042 0.0075 0.0159 1.0000
10.250 1.0887 0.01643 0.01097 0.0088 0.0154 1.0000
10.500 1.1088 0.01691 0.01152 0.0101 0.0148 1.0000
10.750 1.1289 0.01738 0.01203 0.0113 0.0142 1.0000
11.000 1.1497 0.01779 0.01246 0.0124 0.0135 1.0000
11.250 1.1680 0.01841 0.01313 0.0138 0.0130 1.0000
11.500 1.1808 0.01950 0.01429 0.0159 0.0123 1.0000
11.750 1.1953 0.02040 0.01530 0.0178 0.0120 1.0000
12.000 1.2132 0.02100 0.01598 0.0192 0.0117 1.0000
12.250 1.2290 0.02174 0.01680 0.0208 0.0114 1.0000
12.500 1.2439 0.02252 0.01767 0.0225 0.0112 1.0000
12.750 1.2587 0.02327 0.01848 0.0241 0.0108 1.0000
13.000 1.2703 0.02411 0.01940 0.0262 0.0106 1.0000
13.250 1.2773 0.02508 0.02045 0.0288 0.0104 1.0000
13.500 1.2873 0.02591 0.02134 0.0309 0.0101 1.0000
13.750 1.2914 0.02720 0.02272 0.0332 0.0099 1.0000
14.000 1.2944 0.02866 0.02429 0.0352 0.0098 1.0000
14.250 1.2924 0.03067 0.02640 0.0369 0.0096 1.0000
14.500 1.2876 0.03317 0.02905 0.0379 0.0095 1.0000
14.750 1.2781 0.03655 0.03258 0.0379 0.0093 1.0000
15.000 1.2543 0.04230 0.03856 0.0360 0.0092 1.0000
15.250 1.2454 0.04697 0.04339 0.0334 0.0091 1.0000
15.500 1.2449 0.05082 0.04735 0.0309 0.0090 1.0000
15.750 1.2257 0.05779 0.05449 0.0265 0.0091 1.0000
16.000 1.2112 0.06434 0.06119 0.0223 0.0090 1.0000
16.250 1.1902 0.07187 0.06886 0.0178 0.0091 1.0000
16.500 1.1704 0.07930 0.07641 0.0136 0.0090 1.0000
17.000 1.1143 0.09695 0.09430 0.0039 0.0091 1.0000
17.250 1.0865 0.10622 0.10369 -0.0011 0.0091 1.0000
17.500 1.0594 0.11560 0.11319 -0.0061 0.0092 1.0000
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