WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 76-100 (fx76100-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.42 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx76100-il-1000000-n5.txt Download as CSV file: xf-fx76100-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -1.1587 0.10185 0.09907 -0.0017 1.0000 0.0066
-17.500 -1.2067 0.08949 0.08655 -0.0084 1.0000 0.0066
-17.250 -1.2563 0.07703 0.07391 -0.0153 1.0000 0.0064
-17.000 -1.2908 0.06715 0.06386 -0.0210 1.0000 0.0064
-16.750 -1.3230 0.05762 0.05414 -0.0269 1.0000 0.0064
-16.500 -1.3492 0.04945 0.04578 -0.0323 1.0000 0.0063
-16.250 -1.3533 0.04529 0.04149 -0.0347 1.0000 0.0065
-16.000 -1.3617 0.04088 0.03693 -0.0369 1.0000 0.0065
-15.750 -1.3641 0.03769 0.03361 -0.0380 1.0000 0.0066
-15.500 -1.3669 0.03481 0.03061 -0.0385 1.0000 0.0066
-15.250 -1.3684 0.03236 0.02804 -0.0381 1.0000 0.0066
-15.000 -1.3664 0.03048 0.02605 -0.0372 1.0000 0.0067
-14.750 -1.3667 0.02859 0.02404 -0.0357 1.0000 0.0069
-14.500 -1.3620 0.02722 0.02257 -0.0340 1.0000 0.0069
-14.250 -1.3581 0.02589 0.02114 -0.0319 1.0000 0.0072
-14.000 -1.3501 0.02490 0.02006 -0.0297 1.0000 0.0072
-13.750 -1.3432 0.02390 0.01899 -0.0272 1.0000 0.0074
-13.500 -1.3334 0.02307 0.01810 -0.0248 1.0000 0.0076
-13.250 -1.3195 0.02231 0.01726 -0.0231 1.0000 0.0078
-13.000 -1.3047 0.02156 0.01645 -0.0215 1.0000 0.0081
-12.750 -1.2889 0.02086 0.01567 -0.0199 1.0000 0.0083
-12.500 -1.2720 0.02021 0.01495 -0.0184 1.0000 0.0085
-12.250 -1.2546 0.01957 0.01424 -0.0170 1.0000 0.0088
-12.000 -1.2365 0.01896 0.01357 -0.0157 1.0000 0.0089
-11.750 -1.2176 0.01841 0.01296 -0.0144 1.0000 0.0093
-11.500 -1.1996 0.01777 0.01225 -0.0130 1.0000 0.0097
-11.250 -1.1805 0.01720 0.01165 -0.0117 1.0000 0.0101
-11.000 -1.1607 0.01671 0.01112 -0.0104 1.0000 0.0106
-10.750 -1.1407 0.01621 0.01058 -0.0092 1.0000 0.0111
-10.500 -1.1201 0.01577 0.01009 -0.0080 1.0000 0.0116
-10.250 -1.0993 0.01537 0.00964 -0.0068 1.0000 0.0120
-10.000 -1.0789 0.01492 0.00914 -0.0055 1.0000 0.0125
-9.750 -1.0586 0.01447 0.00867 -0.0042 1.0000 0.0132
-9.500 -1.0379 0.01408 0.00826 -0.0030 1.0000 0.0140
-9.250 -1.0171 0.01372 0.00787 -0.0017 1.0000 0.0148
-9.000 -0.9961 0.01340 0.00751 -0.0004 1.0000 0.0154
-8.750 -0.9753 0.01306 0.00714 0.0009 1.0000 0.0160
-8.500 -0.9550 0.01270 0.00678 0.0023 1.0000 0.0173
-8.250 -0.9344 0.01239 0.00646 0.0037 1.0000 0.0185
-8.000 -0.9138 0.01211 0.00615 0.0051 1.0000 0.0195
-7.750 -0.8872 0.01182 0.00583 0.0052 0.9994 0.0205
-7.500 -0.8565 0.01147 0.00549 0.0045 0.9979 0.0223
-7.250 -0.8262 0.01117 0.00518 0.0038 0.9956 0.0241
-7.000 -0.7960 0.01091 0.00490 0.0032 0.9934 0.0254
-6.750 -0.7648 0.01059 0.00459 0.0023 0.9911 0.0282
-6.500 -0.7322 0.01030 0.00431 0.0012 0.9890 0.0310
-6.250 -0.7020 0.01004 0.00405 0.0006 0.9857 0.0339
-6.000 -0.6709 0.00975 0.00379 -0.0002 0.9832 0.0382
-5.750 -0.6391 0.00949 0.00354 -0.0011 0.9814 0.0435
-5.500 -0.6099 0.00924 0.00332 -0.0014 0.9777 0.0491
-5.250 -0.5797 0.00897 0.00310 -0.0020 0.9738 0.0571
-5.000 -0.5470 0.00869 0.00287 -0.0031 0.9710 0.0682
-4.750 -0.5149 0.00842 0.00266 -0.0041 0.9652 0.0819
-4.250 -0.4432 0.00782 0.00224 -0.0078 0.9522 0.1229
-4.000 -0.4085 0.00759 0.00207 -0.0093 0.9457 0.1420
-3.750 -0.3762 0.00736 0.00192 -0.0103 0.9351 0.1614
-3.500 -0.3437 0.00719 0.00178 -0.0113 0.9202 0.1780
-3.250 -0.3141 0.00704 0.00165 -0.0116 0.9023 0.1973
-3.000 -0.2865 0.00693 0.00154 -0.0114 0.8823 0.2139
-2.750 -0.2607 0.00683 0.00143 -0.0109 0.8609 0.2311
-2.500 -0.2362 0.00673 0.00134 -0.0100 0.8339 0.2521
-2.250 -0.2125 0.00667 0.00125 -0.0090 0.8041 0.2729
-2.000 -0.1894 0.00663 0.00117 -0.0078 0.7702 0.2957
-1.750 -0.1662 0.00660 0.00110 -0.0067 0.7370 0.3190
-1.500 -0.1429 0.00658 0.00105 -0.0056 0.7027 0.3415
-1.250 -0.1193 0.00658 0.00101 -0.0046 0.6682 0.3631
-1.000 -0.0957 0.00655 0.00097 -0.0036 0.6367 0.3914
-0.750 -0.0719 0.00658 0.00094 -0.0027 0.6011 0.4152
-0.500 -0.0477 0.00657 0.00092 -0.0018 0.5695 0.4403
-0.250 -0.0240 0.00657 0.00091 -0.0009 0.5341 0.4711
0.000 -0.0001 0.00656 0.00090 0.0000 0.5013 0.5034
0.250 0.0239 0.00655 0.00091 0.0009 0.4733 0.5386
0.500 0.0478 0.00656 0.00092 0.0018 0.4438 0.5713
0.750 0.0718 0.00657 0.00094 0.0027 0.4156 0.6023
1.000 0.0957 0.00658 0.00097 0.0036 0.3881 0.6347
1.250 0.1194 0.00658 0.00101 0.0046 0.3635 0.6674
1.500 0.1430 0.00658 0.00105 0.0056 0.3419 0.7015
1.750 0.1658 0.00660 0.00111 0.0068 0.3164 0.7392
2.000 0.1891 0.00663 0.00117 0.0079 0.2941 0.7721
2.250 0.2126 0.00666 0.00125 0.0090 0.2764 0.8039
2.500 0.2362 0.00674 0.00134 0.0100 0.2518 0.8332
2.750 0.2606 0.00683 0.00143 0.0109 0.2297 0.8604
3.250 0.3140 0.00704 0.00165 0.0116 0.1971 0.9019
3.500 0.3436 0.00720 0.00178 0.0113 0.1773 0.9201
3.750 0.3763 0.00736 0.00192 0.0103 0.1613 0.9352
4.000 0.4083 0.00759 0.00207 0.0093 0.1414 0.9456
4.250 0.4432 0.00781 0.00223 0.0078 0.1238 0.9522
4.500 0.4771 0.00812 0.00244 0.0064 0.1001 0.9599
4.750 0.5150 0.00841 0.00266 0.0041 0.0824 0.9653
5.000 0.5470 0.00871 0.00288 0.0031 0.0667 0.9710
5.250 0.5798 0.00898 0.00310 0.0019 0.0563 0.9739
5.500 0.6100 0.00924 0.00332 0.0014 0.0487 0.9777
5.750 0.6391 0.00951 0.00355 0.0011 0.0425 0.9815
6.000 0.6710 0.00976 0.00380 0.0001 0.0380 0.9833
6.250 0.7021 0.01004 0.00405 -0.0006 0.0338 0.9857
6.500 0.7324 0.01030 0.00432 -0.0012 0.0312 0.9890
6.750 0.7649 0.01059 0.00459 -0.0023 0.0283 0.9911
7.000 0.7961 0.01091 0.00490 -0.0032 0.0253 0.9935
7.250 0.8264 0.01117 0.00519 -0.0038 0.0240 0.9956
7.500 0.8567 0.01147 0.00549 -0.0045 0.0223 0.9980
7.750 0.8873 0.01182 0.00583 -0.0053 0.0206 0.9994
8.000 0.9137 0.01212 0.00616 -0.0051 0.0196 1.0000
8.250 0.9344 0.01239 0.00646 -0.0037 0.0186 1.0000
8.500 0.9550 0.01270 0.00678 -0.0023 0.0175 1.0000
8.750 0.9753 0.01305 0.00714 -0.0009 0.0162 1.0000
9.000 0.9961 0.01339 0.00751 0.0004 0.0154 1.0000
9.250 1.0170 0.01373 0.00788 0.0017 0.0148 1.0000
9.500 1.0380 0.01408 0.00826 0.0030 0.0140 1.0000
9.750 1.0587 0.01447 0.00867 0.0042 0.0134 1.0000
10.000 1.0791 0.01490 0.00912 0.0055 0.0126 1.0000
10.250 1.0995 0.01536 0.00962 0.0068 0.0120 1.0000
10.500 1.1201 0.01578 0.01010 0.0080 0.0116 1.0000
10.750 1.1408 0.01621 0.01058 0.0092 0.0111 1.0000
11.000 1.1611 0.01667 0.01108 0.0104 0.0105 1.0000
11.250 1.1809 0.01718 0.01162 0.0116 0.0101 1.0000
11.500 1.1999 0.01776 0.01223 0.0129 0.0096 1.0000
11.750 1.2179 0.01841 0.01295 0.0143 0.0092 1.0000
12.000 1.2371 0.01892 0.01353 0.0156 0.0089 1.0000
12.250 1.2552 0.01954 0.01421 0.0169 0.0087 1.0000
12.500 1.2727 0.02016 0.01490 0.0183 0.0085 1.0000
12.750 1.2897 0.02081 0.01562 0.0198 0.0081 1.0000
13.000 1.3057 0.02151 0.01638 0.0213 0.0079 1.0000
13.250 1.3203 0.02227 0.01721 0.0230 0.0077 1.0000
13.500 1.3345 0.02304 0.01805 0.0247 0.0075 1.0000
13.750 1.3438 0.02391 0.01899 0.0271 0.0073 1.0000
14.000 1.3521 0.02482 0.01998 0.0295 0.0072 1.0000
14.250 1.3582 0.02593 0.02117 0.0318 0.0070 1.0000
14.500 1.3632 0.02720 0.02254 0.0339 0.0069 1.0000
14.750 1.3658 0.02873 0.02418 0.0357 0.0067 1.0000
15.000 1.3678 0.03044 0.02601 0.0371 0.0067 1.0000
15.250 1.3722 0.03212 0.02778 0.0379 0.0066 1.0000
15.500 1.3747 0.03413 0.02991 0.0384 0.0065 1.0000
15.750 1.3708 0.03706 0.03296 0.0381 0.0065 1.0000
16.000 1.3679 0.04025 0.03629 0.0371 0.0063 1.0000
16.250 1.3615 0.04430 0.04048 0.0351 0.0063 1.0000
16.500 1.3509 0.04942 0.04575 0.0320 0.0063 1.0000
16.750 1.3288 0.05691 0.05342 0.0271 0.0064 1.0000
17.000 1.3054 0.06489 0.06157 0.0222 0.0063 1.0000
17.250 1.2713 0.07474 0.07159 0.0164 0.0063 1.0000
17.500 1.2168 0.08811 0.08515 0.0089 0.0065 1.0000
17.750 1.1664 0.10087 0.09808 0.0020 0.0065 1.0000
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