WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 75-141 (fx75141-il) Reynolds number: 1,000,000 Max Cl/Cd: 120.64 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75141-il-1000000-n5.txt Download as CSV file: xf-fx75141-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 75-141
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
------ -------- --------- --------- -------- -------- --------
-17.500 -0.6674 0.12252 0.11967 -0.0531 0.8149 0.0089
-17.250 -0.7426 0.10353 0.10050 -0.0634 0.8145 0.0088
-17.000 -0.8293 0.08375 0.08046 -0.0751 0.8138 0.0085
-16.500 -0.9185 0.05933 0.05561 -0.0917 0.8097 0.0085
-16.250 -0.9401 0.05172 0.04781 -0.0976 0.8074 0.0084
-16.000 -0.9470 0.04676 0.04272 -0.1018 0.8050 0.0085
-15.750 -0.9497 0.04251 0.03834 -0.1055 0.8025 0.0086
-15.500 -0.9488 0.03878 0.03448 -0.1090 0.8002 0.0087
-15.250 -0.9400 0.03602 0.03160 -0.1120 0.7981 0.0087
-14.750 -0.9193 0.03124 0.02660 -0.1171 0.7943 0.0090
-14.500 -0.9074 0.02933 0.02460 -0.1188 0.7927 0.0091
-14.250 -0.8934 0.02770 0.02288 -0.1204 0.7910 0.0093
-14.000 -0.8796 0.02605 0.02113 -0.1218 0.7892 0.0094
-13.750 -0.8621 0.02484 0.01984 -0.1229 0.7873 0.0096
-13.500 -0.8459 0.02353 0.01844 -0.1240 0.7855 0.0098
-13.250 -0.8277 0.02248 0.01729 -0.1248 0.7838 0.0100
-13.000 -0.8100 0.02147 0.01620 -0.1255 0.7823 0.0101
-12.750 -0.7929 0.02055 0.01519 -0.1258 0.7807 0.0103
-12.500 -0.7806 0.01956 0.01411 -0.1254 0.7791 0.0104
-12.250 -0.7638 0.01872 0.01323 -0.1251 0.7781 0.0108
-12.000 -0.7443 0.01808 0.01254 -0.1248 0.7770 0.0112
-11.750 -0.7238 0.01750 0.01191 -0.1246 0.7758 0.0114
-11.500 -0.7025 0.01696 0.01132 -0.1243 0.7747 0.0117
-11.250 -0.6808 0.01642 0.01074 -0.1240 0.7735 0.0120
-11.000 -0.6583 0.01595 0.01021 -0.1238 0.7722 0.0123
-10.750 -0.6353 0.01550 0.00971 -0.1235 0.7708 0.0126
-10.500 -0.6118 0.01508 0.00922 -0.1233 0.7696 0.0129
-10.250 -0.5881 0.01466 0.00875 -0.1231 0.7685 0.0133
-10.000 -0.5645 0.01418 0.00824 -0.1229 0.7674 0.0138
-9.750 -0.5399 0.01380 0.00783 -0.1228 0.7663 0.0144
-9.500 -0.5147 0.01347 0.00746 -0.1228 0.7652 0.0149
-9.250 -0.4892 0.01315 0.00710 -0.1228 0.7640 0.0155
-9.000 -0.4635 0.01285 0.00676 -0.1227 0.7629 0.0161
-8.750 -0.4379 0.01253 0.00640 -0.1226 0.7620 0.0167
-8.500 -0.4123 0.01218 0.00604 -0.1226 0.7610 0.0175
-8.250 -0.3861 0.01188 0.00574 -0.1226 0.7601 0.0184
-8.000 -0.3597 0.01162 0.00545 -0.1226 0.7590 0.0192
-7.750 -0.3330 0.01138 0.00518 -0.1226 0.7577 0.0201
-7.500 -0.3066 0.01109 0.00489 -0.1226 0.7561 0.0213
-7.250 -0.2800 0.01084 0.00464 -0.1226 0.7544 0.0228
-7.000 -0.2531 0.01063 0.00440 -0.1226 0.7525 0.0242
-6.750 -0.2261 0.01041 0.00415 -0.1226 0.7507 0.0256
-6.500 -0.1990 0.01020 0.00393 -0.1227 0.7488 0.0276
-6.250 -0.1714 0.01003 0.00374 -0.1228 0.7470 0.0295
-6.000 -0.1442 0.00981 0.00354 -0.1228 0.7456 0.0323
-5.750 -0.1167 0.00962 0.00336 -0.1229 0.7441 0.0350
-5.500 -0.0890 0.00944 0.00318 -0.1230 0.7425 0.0378
-5.250 -0.0614 0.00926 0.00302 -0.1231 0.7409 0.0417
-5.000 -0.0336 0.00910 0.00286 -0.1232 0.7391 0.0458
-4.750 -0.0059 0.00893 0.00271 -0.1233 0.7374 0.0508
-4.500 0.0219 0.00876 0.00256 -0.1234 0.7357 0.0578
-4.250 0.0498 0.00861 0.00242 -0.1235 0.7339 0.0654
-4.000 0.0777 0.00847 0.00230 -0.1236 0.7321 0.0751
-3.750 0.1055 0.00829 0.00218 -0.1238 0.7303 0.0909
-3.500 0.1333 0.00810 0.00206 -0.1239 0.7283 0.1090
-3.250 0.1612 0.00791 0.00196 -0.1240 0.7263 0.1308
-3.000 0.1889 0.00770 0.00186 -0.1242 0.7241 0.1608
-2.750 0.2166 0.00750 0.00176 -0.1243 0.7219 0.1932
-2.500 0.2442 0.00730 0.00166 -0.1244 0.7196 0.2288
-2.250 0.2715 0.00705 0.00156 -0.1245 0.7172 0.2794
-2.000 0.2986 0.00676 0.00146 -0.1246 0.7149 0.3439
-1.750 0.3260 0.00651 0.00140 -0.1247 0.7122 0.4051
-1.500 0.3534 0.00631 0.00137 -0.1247 0.7089 0.4589
-1.250 0.3813 0.00621 0.00134 -0.1248 0.7056 0.4890
-1.000 0.4091 0.00614 0.00131 -0.1248 0.7022 0.5107
-0.750 0.4371 0.00609 0.00129 -0.1248 0.6988 0.5262
-0.500 0.4651 0.00602 0.00129 -0.1248 0.6944 0.5494
-0.250 0.4927 0.00597 0.00129 -0.1248 0.6895 0.5722
0.000 0.5202 0.00594 0.00129 -0.1247 0.6846 0.5892
0.250 0.5480 0.00592 0.00132 -0.1246 0.6784 0.6083
0.500 0.5752 0.00592 0.00135 -0.1244 0.6716 0.6281
0.750 0.6027 0.00595 0.00140 -0.1243 0.6638 0.6421
1.000 0.6298 0.00600 0.00141 -0.1241 0.6552 0.6503
1.250 0.6570 0.00605 0.00146 -0.1240 0.6453 0.6559
1.500 0.6835 0.00612 0.00150 -0.1237 0.6340 0.6613
1.750 0.7091 0.00625 0.00155 -0.1232 0.6181 0.6662
2.000 0.7328 0.00643 0.00164 -0.1223 0.5959 0.6703
2.250 0.7563 0.00664 0.00176 -0.1214 0.5714 0.6743
2.500 0.7804 0.00684 0.00187 -0.1206 0.5509 0.6784
2.750 0.8058 0.00700 0.00197 -0.1202 0.5374 0.6821
3.000 0.8315 0.00712 0.00208 -0.1197 0.5278 0.6852
3.250 0.8567 0.00726 0.00220 -0.1192 0.5161 0.6882
3.500 0.8820 0.00740 0.00232 -0.1188 0.5037 0.6913
3.750 0.9068 0.00757 0.00244 -0.1182 0.4907 0.6944
4.000 0.9313 0.00774 0.00258 -0.1176 0.4772 0.6975
4.250 0.9555 0.00792 0.00272 -0.1169 0.4637 0.6999
4.500 0.9769 0.00821 0.00292 -0.1157 0.4382 0.7023
4.750 0.9937 0.00869 0.00320 -0.1136 0.3936 0.7048
5.000 1.0076 0.00930 0.00356 -0.1111 0.3424 0.7076
5.250 1.0218 0.00988 0.00392 -0.1087 0.2972 0.7103
5.500 1.0363 0.01044 0.00429 -0.1063 0.2584 0.7127
5.750 1.0505 0.01098 0.00465 -0.1039 0.2236 0.7149
6.000 1.0662 0.01139 0.00497 -0.1017 0.2011 0.7172
6.250 1.0807 0.01173 0.00525 -0.0992 0.1836 0.7195
6.500 1.0944 0.01212 0.00557 -0.0967 0.1661 0.7218
6.750 1.1093 0.01251 0.00591 -0.0944 0.1513 0.7241
7.000 1.1236 0.01291 0.00626 -0.0920 0.1376 0.7265
7.250 1.1374 0.01335 0.00663 -0.0896 0.1238 0.7290
7.750 1.1611 0.01437 0.00754 -0.0844 0.0939 0.7350
8.000 1.1717 0.01495 0.00807 -0.0817 0.0804 0.7387
8.250 1.1835 0.01552 0.00860 -0.0793 0.0703 0.7421
8.500 1.1945 0.01617 0.00920 -0.0769 0.0601 0.7447
8.750 1.2065 0.01681 0.00982 -0.0748 0.0530 0.7468
9.000 1.2193 0.01742 0.01044 -0.0728 0.0479 0.7489
9.250 1.2326 0.01805 0.01108 -0.0710 0.0437 0.7511
9.500 1.2458 0.01871 0.01175 -0.0693 0.0401 0.7537
9.750 1.2591 0.01940 0.01245 -0.0676 0.0372 0.7563
10.000 1.2731 0.02008 0.01315 -0.0661 0.0345 0.7588
10.250 1.2857 0.02086 0.01393 -0.0645 0.0315 0.7612
10.750 1.3127 0.02236 0.01549 -0.0616 0.0276 0.7662
11.000 1.3254 0.02318 0.01633 -0.0601 0.0261 0.7693
11.250 1.3383 0.02401 0.01720 -0.0587 0.0248 0.7728
11.500 1.3515 0.02483 0.01808 -0.0574 0.0236 0.7764
11.750 1.3640 0.02572 0.01900 -0.0561 0.0225 0.7799
12.000 1.3756 0.02668 0.01999 -0.0547 0.0212 0.7841
12.250 1.3872 0.02766 0.02102 -0.0534 0.0203 0.7887
12.500 1.3993 0.02863 0.02204 -0.0522 0.0192 0.7937
12.750 1.4109 0.02964 0.02312 -0.0509 0.0184 0.8001
13.000 1.4214 0.03075 0.02429 -0.0497 0.0176 0.8078
13.250 1.4314 0.03192 0.02552 -0.0485 0.0167 0.8189
13.500 1.4420 0.03307 0.02678 -0.0474 0.0161 0.8390
13.750 1.4697 0.03442 0.02837 -0.0500 0.0154 0.9080
14.000 1.5211 0.03663 0.03068 -0.0583 0.0139 0.9536
14.500 1.5379 0.03970 0.03383 -0.0562 0.0129 1.0000
14.750 1.5465 0.04129 0.03548 -0.0554 0.0125 1.0000
15.000 1.5546 0.04292 0.03716 -0.0545 0.0120 1.0000
15.250 1.5616 0.04470 0.03900 -0.0537 0.0117 1.0000
15.500 1.5679 0.04656 0.04092 -0.0530 0.0112 1.0000
15.750 1.5734 0.04857 0.04298 -0.0522 0.0109 1.0000
16.000 1.5776 0.05073 0.04519 -0.0516 0.0105 1.0000
16.250 1.5819 0.05289 0.04742 -0.0509 0.0101 1.0000
16.500 1.5861 0.05511 0.04971 -0.0504 0.0100 1.0000
16.750 1.5897 0.05743 0.05210 -0.0499 0.0097 1.0000
17.000 1.5928 0.05985 0.05459 -0.0495 0.0094 1.0000
17.250 1.5949 0.06241 0.05722 -0.0492 0.0091 1.0000
17.500 1.5954 0.06514 0.06003 -0.0489 0.0090 1.0000
17.750 1.5951 0.06803 0.06300 -0.0487 0.0087 1.0000
18.000 1.5941 0.07104 0.06608 -0.0486 0.0085 1.0000
18.250 1.5915 0.07431 0.06942 -0.0486 0.0083 1.0000
18.500 1.5882 0.07771 0.07290 -0.0487 0.0081 1.0000
18.750 1.5835 0.08133 0.07660 -0.0490 0.0079 1.0000
19.000 1.5794 0.08492 0.08029 -0.0494 0.0078 1.0000
19.250 1.5753 0.08861 0.08407 -0.0499 0.0077 1.0000
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