FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 75-VG-166/22 (fx75vg166-il) Reynolds number: 100,000 Max Cl/Cd: 25.73 at α=10.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75vg166-il-100000-n5.txt Download as CSV file: xf-fx75vg166-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 75-VG-166/22
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.000 -0.3172 0.10052 0.09444 -0.0952 0.8151 0.0294
-12.750 -0.3225 0.09410 0.08804 -0.0987 0.8143 0.0292
-12.500 -0.3319 0.08686 0.08082 -0.1031 0.8135 0.0288
-12.250 -0.3538 0.07857 0.07248 -0.1086 0.8128 0.0285
-12.000 -0.3740 0.07253 0.06635 -0.1121 0.8120 0.0281
-11.750 -0.4023 0.06676 0.06043 -0.1142 0.8111 0.0279
-11.500 -0.4226 0.06272 0.05623 -0.1144 0.8100 0.0277
-11.250 -0.4421 0.05917 0.05249 -0.1134 0.8087 0.0276
-10.750 -0.4787 0.05284 0.04571 -0.1089 0.8062 0.0277
-10.500 -0.4888 0.05040 0.04307 -0.1062 0.8050 0.0276
-10.250 -0.5006 0.04793 0.04035 -0.1028 0.8036 0.0278
-10.000 -0.5093 0.04593 0.03807 -0.0990 0.8021 0.0281
-9.750 -0.5118 0.04396 0.03580 -0.0958 0.8004 0.0282
-9.500 -0.5105 0.04175 0.03321 -0.0928 0.7987 0.0287
-9.250 -0.5050 0.03985 0.03086 -0.0901 0.7972 0.0294
-9.000 -0.4904 0.03848 0.02941 -0.0891 0.7960 0.0305
-8.750 -0.4753 0.03749 0.02833 -0.0879 0.7949 0.0318
-8.500 -0.4578 0.03620 0.02682 -0.0868 0.7938 0.0332
-8.250 -0.4359 0.03471 0.02503 -0.0861 0.7928 0.0346
-8.000 -0.4104 0.03328 0.02329 -0.0859 0.7917 0.0359
-7.750 -0.3861 0.03211 0.02218 -0.0860 0.7906 0.0377
-7.500 -0.3643 0.03133 0.02136 -0.0855 0.7892 0.0404
-7.250 -0.3391 0.03047 0.02036 -0.0853 0.7876 0.0430
-7.000 -0.3134 0.02949 0.01937 -0.0852 0.7860 0.0450
-6.750 -0.2949 0.02893 0.01883 -0.0842 0.7843 0.0484
-6.500 -0.2759 0.02844 0.01826 -0.0830 0.7828 0.0522
-6.250 -0.2604 0.02789 0.01772 -0.0813 0.7815 0.0558
-6.000 -0.2449 0.02750 0.01728 -0.0796 0.7802 0.0605
-5.750 -0.2297 0.02710 0.01687 -0.0778 0.7791 0.0675
-5.500 -0.2172 0.02685 0.01662 -0.0757 0.7771 0.0763
-5.250 -0.2051 0.02653 0.01640 -0.0736 0.7748 0.0896
-5.000 -0.1923 0.02613 0.01621 -0.0715 0.7725 0.1182
-4.750 -0.1802 0.02560 0.01608 -0.0693 0.7705 0.1888
-4.500 -0.1776 0.02484 0.01607 -0.0656 0.7686 0.3249
-4.250 -0.1043 0.02653 0.01933 -0.0678 0.7687 0.6459
-4.000 -0.0943 0.02731 0.02002 -0.0640 0.7669 0.6857
-3.750 -0.1090 0.02782 0.02052 -0.0571 0.7630 0.7126
-3.500 -0.0951 0.02907 0.02170 -0.0538 0.7601 0.7392
-3.250 -0.0884 0.03008 0.02261 -0.0495 0.7572 0.7628
-3.000 -0.0558 0.03126 0.02365 -0.0488 0.7557 0.7819
-2.750 -0.0279 0.03184 0.02409 -0.0482 0.7544 0.7944
-2.500 -0.0141 0.03219 0.02432 -0.0457 0.7528 0.8060
-2.250 0.0039 0.03270 0.02479 -0.0444 0.7490 0.8121
-2.000 0.0056 0.03300 0.02504 -0.0402 0.7450 0.8221
-1.750 0.0328 0.03315 0.02509 -0.0403 0.7430 0.8273
-1.500 0.0404 0.03325 0.02510 -0.0370 0.7408 0.8356
-1.250 0.0733 0.03331 0.02506 -0.0381 0.7396 0.8388
-1.000 0.0465 0.03383 0.02562 -0.0295 0.7326 0.8499
-0.750 0.0708 0.03393 0.02564 -0.0293 0.7296 0.8530
-0.500 0.0941 0.03395 0.02558 -0.0288 0.7273 0.8566
-0.250 0.1126 0.03389 0.02544 -0.0274 0.7254 0.8613
0.000 0.0915 0.03433 0.02591 -0.0199 0.7174 0.8688
0.250 0.1101 0.03439 0.02592 -0.0187 0.7143 0.8728
0.500 0.1258 0.03436 0.02582 -0.0170 0.7122 0.8765
1.000 0.1133 0.03462 0.02606 -0.0068 0.7005 0.8855
1.250 0.1372 0.03460 0.02599 -0.0065 0.6985 0.8878
1.500 0.1641 0.03454 0.02588 -0.0065 0.6970 0.8906
1.750 0.1324 0.03484 0.02620 0.0022 0.6865 0.8968
2.000 0.1617 0.03477 0.02608 0.0017 0.6845 0.8982
2.500 0.1757 0.03510 0.02640 0.0068 0.6726 0.9030
2.750 0.2026 0.03504 0.02632 0.0067 0.6704 0.9041
3.000 0.2324 0.03495 0.02621 0.0061 0.6688 0.9050
3.250 0.2191 0.03552 0.02678 0.0111 0.6584 0.9089
3.500 0.2472 0.03546 0.02674 0.0107 0.6560 0.9098
3.750 0.2786 0.03535 0.02663 0.0100 0.6542 0.9104
4.000 0.2768 0.03590 0.02721 0.0131 0.6439 0.9125
4.250 0.3071 0.03571 0.02704 0.0126 0.6411 0.9136
4.500 0.3398 0.03550 0.02686 0.0118 0.6392 0.9145
4.750 0.3404 0.03616 0.02755 0.0144 0.6285 0.9167
5.000 0.3712 0.03599 0.02742 0.0137 0.6260 0.9177
5.500 0.4052 0.03650 0.02803 0.0154 0.6128 0.9201
5.750 0.4370 0.03624 0.02783 0.0147 0.6104 0.9205
6.000 0.4430 0.03696 0.02860 0.0164 0.5996 0.9218
6.250 0.4730 0.03673 0.02844 0.0160 0.5961 0.9223
6.500 0.5071 0.03628 0.02808 0.0152 0.5938 0.9227
7.000 0.5488 0.03626 0.02823 0.0162 0.5783 0.9247
7.250 0.5604 0.03670 0.02876 0.0174 0.5661 0.9260
7.500 0.5970 0.03573 0.02790 0.0168 0.5625 0.9265
7.750 0.6109 0.03607 0.02833 0.0178 0.5500 0.9274
8.000 0.6314 0.03597 0.02833 0.0184 0.5389 0.9281
8.250 0.6642 0.03506 0.02754 0.0182 0.5320 0.9286
8.500 0.6813 0.03534 0.02793 0.0188 0.5185 0.9294
8.750 0.7031 0.03536 0.02806 0.0192 0.5062 0.9302
9.000 0.7316 0.03488 0.02771 0.0191 0.4949 0.9308
9.250 0.7617 0.03424 0.02716 0.0191 0.4807 0.9314
9.500 0.7855 0.03407 0.02706 0.0194 0.4605 0.9321
9.750 0.8127 0.03365 0.02667 0.0196 0.4358 0.9328
10.000 0.8405 0.03314 0.02606 0.0200 0.4018 0.9334
10.250 0.8592 0.03339 0.02614 0.0208 0.3620 0.9341
10.500 0.8698 0.03424 0.02670 0.0220 0.3160 0.9350
10.750 0.8756 0.03560 0.02783 0.0233 0.2731 0.9361
11.250 0.8837 0.03898 0.03076 0.0253 0.2009 0.9383
11.500 0.8927 0.04052 0.03223 0.0257 0.1756 0.9393
11.750 0.8997 0.04225 0.03385 0.0261 0.1530 0.9402
12.000 0.9087 0.04389 0.03547 0.0264 0.1320 0.9410
12.250 0.9167 0.04566 0.03720 0.0267 0.1133 0.9418
12.500 0.9235 0.04759 0.03907 0.0269 0.0960 0.9427
12.750 0.9309 0.04952 0.04097 0.0270 0.0813 0.9438
13.000 0.9376 0.05157 0.04302 0.0272 0.0711 0.9452
13.250 0.9448 0.05362 0.04510 0.0272 0.0622 0.9464
13.500 0.9505 0.05587 0.04736 0.0272 0.0560 0.9477
13.750 0.9571 0.05810 0.04967 0.0271 0.0508 0.9491
14.000 0.9634 0.06039 0.05203 0.0269 0.0477 0.9506
14.250 0.9715 0.06257 0.05433 0.0266 0.0445 0.9520
14.500 0.9772 0.06504 0.05685 0.0262 0.0418 0.9535
14.750 0.9840 0.06743 0.05932 0.0258 0.0395 0.9550
15.000 0.9932 0.06958 0.06163 0.0255 0.0377 0.9564
15.250 1.0005 0.07200 0.06418 0.0249 0.0357 0.9580
15.500 1.0068 0.07448 0.06673 0.0243 0.0343 0.9599
15.750 1.0133 0.07693 0.06923 0.0238 0.0330 0.9621
16.250 1.0266 0.08190 0.07460 0.0228 0.0307 0.9717
16.500 1.0307 0.08461 0.07748 0.0220 0.0296 0.9873
16.750 1.0387 0.08774 0.08078 0.0204 0.0288 0.9951
17.000 1.0353 0.09022 0.08334 0.0217 0.0284 1.0000
17.250 1.0396 0.09317 0.08635 0.0209 0.0277 1.0000
17.500 1.0441 0.09613 0.08941 0.0201 0.0273 1.0000
17.750 1.0403 0.10050 0.09402 0.0186 0.0269 1.0000
18.000 1.0318 0.10571 0.09952 0.0164 0.0265 1.0000
18.250 1.0221 0.11125 0.10532 0.0138 0.0263 1.0000
18.500 1.0092 0.11758 0.11190 0.0105 0.0260 1.0000
18.750 0.9954 0.12432 0.11889 0.0068 0.0260 1.0000
19.000 0.9755 0.13262 0.12743 0.0019 0.0258 1.0000
19.250 0.9517 0.14228 0.13734 -0.0041 0.0260 1.0000
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