WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 76-100 (fx76100-il) Reynolds number: 500,000 Max Cl/Cd: 62.87 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx76100-il-500000.txt Download as CSV file: xf-fx76100-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.500 -0.9311 0.10389 0.10113 -0.0041 1.0000 0.0155
-15.250 -0.9741 0.09082 0.08789 -0.0120 1.0000 0.0152
-15.000 -1.0060 0.08044 0.07735 -0.0186 1.0000 0.0150
-14.750 -1.0316 0.07132 0.06805 -0.0250 1.0000 0.0152
-14.500 -1.0540 0.06350 0.06004 -0.0302 1.0000 0.0149
-14.250 -1.0677 0.05742 0.05378 -0.0346 1.0000 0.0152
-14.000 -1.0826 0.05179 0.04797 -0.0378 1.0000 0.0149
-13.750 -1.0970 0.04676 0.04272 -0.0403 1.0000 0.0151
-13.500 -1.1049 0.04312 0.03888 -0.0413 1.0000 0.0153
-13.250 -1.1091 0.04032 0.03590 -0.0414 1.0000 0.0154
-13.000 -1.1077 0.03855 0.03396 -0.0408 1.0000 0.0157
-12.750 -1.1131 0.03593 0.03114 -0.0392 1.0000 0.0157
-12.500 -1.1258 0.03259 0.02759 -0.0365 1.0000 0.0162
-12.250 -1.1246 0.03089 0.02580 -0.0340 1.0000 0.0166
-12.000 -1.1202 0.02960 0.02440 -0.0314 1.0000 0.0168
-11.750 -1.1122 0.02876 0.02353 -0.0289 1.0000 0.0174
-11.500 -1.1022 0.02764 0.02230 -0.0268 1.0000 0.0178
-11.250 -1.0907 0.02653 0.02108 -0.0248 1.0000 0.0183
-11.000 -1.0774 0.02555 0.01998 -0.0229 1.0000 0.0190
-10.750 -1.0638 0.02445 0.01874 -0.0209 1.0000 0.0195
-10.500 -1.0472 0.02375 0.01789 -0.0193 1.0000 0.0200
-10.250 -1.0388 0.02185 0.01589 -0.0167 1.0000 0.0211
-10.000 -1.0228 0.02101 0.01501 -0.0150 1.0000 0.0218
-9.750 -1.0050 0.02034 0.01429 -0.0135 1.0000 0.0227
-9.500 -0.9862 0.01975 0.01363 -0.0120 1.0000 0.0240
-9.250 -0.9666 0.01922 0.01301 -0.0106 1.0000 0.0251
-9.000 -0.9509 0.01822 0.01191 -0.0087 1.0000 0.0262
-8.750 -0.9350 0.01733 0.01100 -0.0068 1.0000 0.0277
-8.500 -0.9155 0.01682 0.01047 -0.0053 1.0000 0.0294
-8.250 -0.8959 0.01632 0.00991 -0.0038 1.0000 0.0308
-8.000 -0.8748 0.01599 0.00950 -0.0025 1.0000 0.0323
-7.750 -0.8605 0.01499 0.00848 -0.0001 1.0000 0.0349
-7.500 -0.8409 0.01454 0.00802 0.0014 1.0000 0.0371
-7.250 -0.8210 0.01416 0.00758 0.0029 1.0000 0.0392
-7.000 -0.8029 0.01360 0.00698 0.0048 1.0000 0.0419
-6.750 -0.7844 0.01311 0.00649 0.0066 1.0000 0.0455
-6.500 -0.7644 0.01278 0.00612 0.0081 1.0000 0.0490
-6.250 -0.7463 0.01228 0.00561 0.0100 1.0000 0.0539
-6.000 -0.7267 0.01194 0.00527 0.0116 1.0000 0.0600
-5.750 -0.7080 0.01150 0.00488 0.0133 1.0000 0.0691
-5.500 -0.6890 0.01110 0.00453 0.0150 1.0000 0.0823
-5.250 -0.6702 0.01070 0.00424 0.0167 1.0000 0.1032
-5.000 -0.6509 0.01034 0.00401 0.0183 1.0000 0.1298
-4.750 -0.6309 0.01008 0.00384 0.0197 1.0000 0.1545
-4.500 -0.6107 0.00984 0.00370 0.0211 1.0000 0.1766
-4.250 -0.5762 0.00964 0.00357 0.0195 0.9977 0.2012
-4.000 -0.5395 0.00940 0.00344 0.0175 0.9946 0.2256
-3.750 -0.5006 0.00916 0.00329 0.0150 0.9907 0.2512
-3.500 -0.4618 0.00890 0.00314 0.0126 0.9869 0.2789
-3.250 -0.4257 0.00863 0.00300 0.0107 0.9831 0.3112
-3.000 -0.3884 0.00835 0.00286 0.0086 0.9803 0.3472
-2.750 -0.3547 0.00804 0.00272 0.0073 0.9747 0.3886
-2.500 -0.3152 0.00766 0.00256 0.0047 0.9712 0.4418
-2.250 -0.2830 0.00731 0.00242 0.0039 0.9645 0.4941
-2.000 -0.2453 0.00694 0.00228 0.0018 0.9604 0.5521
-1.750 -0.2117 0.00663 0.00216 0.0008 0.9534 0.6026
-1.500 -0.1770 0.00633 0.00206 -0.0004 0.9464 0.6518
-1.250 -0.1473 0.00610 0.00198 -0.0005 0.9361 0.6958
-1.000 -0.1161 0.00589 0.00192 -0.0009 0.9254 0.7378
-0.750 -0.0856 0.00573 0.00188 -0.0010 0.9132 0.7761
-0.500 -0.0566 0.00562 0.00186 -0.0008 0.8984 0.8088
-0.250 -0.0287 0.00556 0.00185 -0.0003 0.8811 0.8370
0.000 0.0000 0.00554 0.00185 0.0000 0.8603 0.8600
0.250 0.0287 0.00556 0.00185 0.0003 0.8367 0.8810
0.500 0.0568 0.00562 0.00185 0.0007 0.8077 0.8978
0.750 0.0856 0.00573 0.00188 0.0010 0.7762 0.9133
1.000 0.1160 0.00589 0.00192 0.0009 0.7390 0.9262
1.250 0.1474 0.00610 0.00198 0.0005 0.6961 0.9362
1.500 0.1769 0.00634 0.00205 0.0005 0.6510 0.9464
1.750 0.2118 0.00664 0.00217 -0.0008 0.6025 0.9535
2.000 0.2454 0.00694 0.00228 -0.0019 0.5510 0.9604
2.250 0.2830 0.00731 0.00242 -0.0039 0.4922 0.9645
2.500 0.3151 0.00765 0.00257 -0.0047 0.4438 0.9712
2.750 0.3548 0.00804 0.00272 -0.0073 0.3885 0.9747
3.000 0.3884 0.00835 0.00286 -0.0085 0.3471 0.9802
3.250 0.4254 0.00863 0.00300 -0.0106 0.3111 0.9831
3.500 0.4619 0.00891 0.00314 -0.0126 0.2779 0.9869
3.750 0.5006 0.00916 0.00329 -0.0150 0.2511 0.9908
4.000 0.5394 0.00941 0.00344 -0.0174 0.2250 0.9946
4.250 0.5763 0.00963 0.00357 -0.0195 0.2013 0.9977
4.500 0.6106 0.00984 0.00370 -0.0211 0.1765 1.0000
4.750 0.6308 0.01007 0.00384 -0.0197 0.1549 1.0000
5.000 0.6507 0.01035 0.00401 -0.0182 0.1292 1.0000
5.250 0.6699 0.01071 0.00424 -0.0166 0.1021 1.0000
5.500 0.6889 0.01110 0.00453 -0.0150 0.0818 1.0000
5.750 0.7079 0.01150 0.00488 -0.0133 0.0688 1.0000
6.000 0.7265 0.01194 0.00528 -0.0115 0.0597 1.0000
6.250 0.7461 0.01228 0.00562 -0.0099 0.0538 1.0000
6.500 0.7643 0.01278 0.00613 -0.0081 0.0489 1.0000
6.750 0.7842 0.01312 0.00651 -0.0065 0.0457 1.0000
7.000 0.8027 0.01361 0.00700 -0.0047 0.0422 1.0000
7.250 0.8204 0.01421 0.00764 -0.0028 0.0394 1.0000
7.500 0.8408 0.01455 0.00802 -0.0014 0.0371 1.0000
7.750 0.8604 0.01499 0.00849 0.0002 0.0349 1.0000
8.000 0.8746 0.01600 0.00950 0.0025 0.0322 1.0000
8.250 0.8957 0.01633 0.00992 0.0038 0.0309 1.0000
8.500 0.9155 0.01682 0.01046 0.0053 0.0294 1.0000
8.750 0.9349 0.01734 0.01102 0.0068 0.0278 1.0000
9.000 0.9519 0.01811 0.01181 0.0085 0.0264 1.0000
9.250 0.9662 0.01928 0.01306 0.0107 0.0252 1.0000
9.500 0.9866 0.01970 0.01358 0.0120 0.0240 1.0000
9.750 1.0053 0.02032 0.01427 0.0134 0.0228 1.0000
10.000 1.0230 0.02099 0.01499 0.0149 0.0219 1.0000
10.250 1.0388 0.02186 0.01589 0.0167 0.0209 1.0000
10.500 1.0472 0.02379 0.01793 0.0193 0.0200 1.0000
10.750 1.0641 0.02446 0.01874 0.0209 0.0195 1.0000
11.000 1.0782 0.02546 0.01989 0.0228 0.0189 1.0000
11.250 1.0915 0.02646 0.02100 0.0246 0.0183 1.0000
11.500 1.1027 0.02762 0.02228 0.0267 0.0178 1.0000
11.750 1.1135 0.02863 0.02337 0.0287 0.0172 1.0000
12.000 1.1215 0.02951 0.02431 0.0312 0.0168 1.0000
12.250 1.1251 0.03087 0.02575 0.0339 0.0164 1.0000
12.500 1.1251 0.03270 0.02769 0.0365 0.0160 1.0000
12.750 1.1160 0.03556 0.03078 0.0390 0.0156 1.0000
13.000 1.1172 0.03731 0.03270 0.0403 0.0154 1.0000
13.250 1.1120 0.04003 0.03562 0.0411 0.0153 1.0000
13.500 1.1079 0.04285 0.03862 0.0411 0.0151 1.0000
13.750 1.0972 0.04690 0.04287 0.0400 0.0150 1.0000
14.000 1.0880 0.05120 0.04735 0.0378 0.0149 1.0000
14.250 1.0744 0.05668 0.05303 0.0344 0.0148 1.0000
14.500 1.0556 0.06353 0.06008 0.0299 0.0149 1.0000
14.750 1.0345 0.07131 0.06805 0.0245 0.0149 1.0000
15.000 1.0046 0.08113 0.07807 0.0178 0.0150 1.0000
15.250 0.9736 0.09145 0.08854 0.0112 0.0151 1.0000
15.500 0.9361 0.10368 0.10094 0.0036 0.0152 1.0000
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