WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il) Reynolds number: 50,000 Max Cl/Cd: 14.17 at α=13° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05188-il-50000-n5.txt Download as CSV file: xf-fx05188-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-188 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.000 -0.4142 0.11483 0.10775 -0.0701 1.0000 0.0571
-12.750 -0.4367 0.11114 0.10416 -0.0691 1.0000 0.0567
-12.500 -0.4645 0.10694 0.10002 -0.0684 1.0000 0.0561
-12.250 -0.4874 0.09710 0.09009 -0.0756 0.9937 0.0552
-12.000 -0.5167 0.08809 0.08090 -0.0824 0.9863 0.0545
-11.750 -0.5420 0.08121 0.07380 -0.0872 0.9783 0.0539
-11.500 -0.5624 0.07566 0.06798 -0.0906 0.9711 0.0537
-11.250 -0.5785 0.07138 0.06345 -0.0925 0.9631 0.0537
-11.000 -0.5907 0.06769 0.05947 -0.0936 0.9557 0.0538
-10.750 -0.5984 0.06458 0.05609 -0.0942 0.9484 0.0542
-10.500 -0.6053 0.06198 0.05321 -0.0937 0.9411 0.0545
-10.250 -0.6098 0.05969 0.05063 -0.0927 0.9340 0.0551
-10.000 -0.6038 0.05713 0.04772 -0.0928 0.9291 0.0556
-9.750 -0.6045 0.05538 0.04572 -0.0905 0.9216 0.0560
-9.500 -0.5889 0.05306 0.04306 -0.0905 0.9171 0.0566
-9.250 -0.5622 0.05077 0.04038 -0.0917 0.9142 0.0574
-9.000 -0.5477 0.04942 0.03875 -0.0901 0.9090 0.0581
-8.750 -0.5123 0.04789 0.03709 -0.0909 0.9060 0.0594
-8.500 -0.4677 0.04658 0.03577 -0.0930 0.9041 0.0627
-8.250 -0.4162 0.04560 0.03456 -0.0953 0.9027 0.0669
-8.000 -0.3669 0.04488 0.03379 -0.0970 0.9012 0.0709
-7.750 -0.3336 0.04411 0.03297 -0.0978 0.8986 0.0748
-7.500 -0.3130 0.04346 0.03220 -0.0972 0.8946 0.0794
-7.250 -0.3147 0.04309 0.03186 -0.0935 0.8874 0.0828
-7.000 -0.3023 0.04222 0.03099 -0.0926 0.8827 0.0892
-6.750 -0.2890 0.04106 0.02987 -0.0921 0.8791 0.0993
-6.500 -0.3104 0.04110 0.02993 -0.0852 0.8699 0.1026
-6.250 -0.3097 0.04013 0.02904 -0.0826 0.8647 0.1144
-6.000 -0.3227 0.03953 0.02853 -0.0776 0.8581 0.1271
-5.750 -0.3380 0.03882 0.02798 -0.0724 0.8506 0.1466
-5.500 -0.3461 0.03683 0.02665 -0.0697 0.8457 0.2233
-5.250 -0.3691 0.03619 0.02655 -0.0630 0.8377 0.2885
-5.000 -0.3530 0.03771 0.02920 -0.0573 0.8334 0.4855
-4.750 -0.3314 0.03990 0.03137 -0.0536 0.8295 0.5703
-4.500 -0.2792 0.04576 0.03704 -0.0489 0.8277 0.6339
-4.250 -0.2905 0.04673 0.03797 -0.0421 0.8197 0.6481
-4.000 -0.2684 0.04735 0.03839 -0.0404 0.8154 0.6616
-3.750 -0.2467 0.04717 0.03797 -0.0400 0.8120 0.6723
-3.500 -0.2613 0.04703 0.03777 -0.0346 0.8047 0.6837
-3.250 -0.2426 0.04722 0.03780 -0.0331 0.7999 0.6897
-3.000 -0.2269 0.04676 0.03714 -0.0325 0.7960 0.7002
-2.750 -0.2112 0.04691 0.03716 -0.0307 0.7914 0.7058
-2.500 -0.2131 0.04689 0.03705 -0.0270 0.7849 0.7145
-2.250 -0.1930 0.04672 0.03672 -0.0265 0.7809 0.7214
-2.000 -0.1633 0.04663 0.03645 -0.0271 0.7782 0.7277
-1.750 -0.1772 0.04664 0.03643 -0.0220 0.7701 0.7367
-1.500 -0.1564 0.04671 0.03638 -0.0212 0.7661 0.7423
-1.250 -0.1340 0.04642 0.03592 -0.0216 0.7628 0.7509
-1.000 -0.1328 0.04671 0.03618 -0.0180 0.7560 0.7566
-0.750 -0.1180 0.04673 0.03610 -0.0168 0.7513 0.7639
-0.500 -0.0942 0.04664 0.03588 -0.0169 0.7479 0.7707
-0.250 -0.0842 0.04684 0.03602 -0.0149 0.7425 0.7769
0.000 -0.0750 0.04688 0.03598 -0.0135 0.7365 0.7848
0.250 -0.0509 0.04692 0.03594 -0.0132 0.7328 0.7895
0.500 -0.0218 0.04687 0.03578 -0.0140 0.7300 0.7954
0.750 -0.0254 0.04722 0.03612 -0.0109 0.7217 0.8020
1.000 -0.0033 0.04730 0.03613 -0.0106 0.7173 0.8068
1.250 0.0258 0.04728 0.03602 -0.0116 0.7142 0.8123
1.750 0.0484 0.04786 0.03654 -0.0088 0.7014 0.8228
2.000 0.0771 0.04790 0.03652 -0.0097 0.6979 0.8280
2.500 0.1023 0.04860 0.03719 -0.0074 0.6849 0.8380
2.750 0.1307 0.04872 0.03728 -0.0082 0.6812 0.8429
3.250 0.1581 0.04961 0.03817 -0.0065 0.6684 0.8524
3.500 0.1864 0.04977 0.03831 -0.0072 0.6645 0.8571
4.000 0.2155 0.05084 0.03942 -0.0060 0.6516 0.8664
4.250 0.2443 0.05101 0.03960 -0.0067 0.6479 0.8709
4.500 0.2524 0.05189 0.04052 -0.0058 0.6397 0.8759
4.750 0.2750 0.05226 0.04092 -0.0060 0.6346 0.8802
5.000 0.3050 0.05239 0.04108 -0.0066 0.6313 0.8846
5.250 0.3083 0.05352 0.04228 -0.0054 0.6218 0.8895
5.500 0.3365 0.05382 0.04263 -0.0063 0.6176 0.8939
5.750 0.3463 0.05473 0.04359 -0.0053 0.6099 0.8986
6.000 0.3677 0.05528 0.04421 -0.0056 0.6040 0.9032
6.250 0.3999 0.05549 0.04449 -0.0068 0.6006 0.9078
6.500 0.4021 0.05681 0.04591 -0.0055 0.5906 0.9126
6.750 0.4303 0.05712 0.04630 -0.0063 0.5862 0.9173
7.000 0.4404 0.05836 0.04763 -0.0060 0.5776 0.9224
7.250 0.4634 0.05887 0.04825 -0.0063 0.5717 0.9275
7.500 0.4976 0.05890 0.04839 -0.0075 0.5682 0.9326
7.750 0.4992 0.06069 0.05029 -0.0069 0.5569 0.9379
8.000 0.5328 0.06074 0.05049 -0.0080 0.5526 0.9434
8.250 0.5380 0.06250 0.05237 -0.0078 0.5417 0.9496
8.500 0.5714 0.06265 0.05268 -0.0092 0.5367 0.9559
8.750 0.5807 0.06437 0.05455 -0.0096 0.5258 0.9635
9.000 0.6153 0.06444 0.05479 -0.0112 0.5202 0.9736
9.500 0.6600 0.06576 0.05643 -0.0129 0.5031 1.0000
9.750 0.6688 0.06756 0.05836 -0.0133 0.4904 1.0000
10.000 0.7105 0.06677 0.05775 -0.0146 0.4852 1.0000
10.250 0.7208 0.06843 0.05956 -0.0151 0.4719 1.0000
10.750 0.7591 0.07003 0.06151 -0.0161 0.4475 1.0000
11.000 0.8063 0.06725 0.05894 -0.0162 0.4374 1.0000
11.500 0.8548 0.06594 0.05800 -0.0159 0.4056 1.0000
11.750 0.8749 0.06615 0.05840 -0.0159 0.3897 1.0000
12.000 0.8969 0.06616 0.05862 -0.0160 0.3729 1.0000
12.250 0.9112 0.06712 0.05974 -0.0161 0.3521 1.0000
12.500 0.9266 0.06791 0.06067 -0.0161 0.3267 1.0000
12.750 0.9497 0.06741 0.06013 -0.0156 0.2901 1.0000
13.000 0.9637 0.06803 0.06039 -0.0151 0.2420 1.0000
13.250 0.9658 0.07057 0.06256 -0.0151 0.2019 1.0000
13.500 0.9656 0.07374 0.06545 -0.0155 0.1735 1.0000
13.750 0.9658 0.07707 0.06857 -0.0161 0.1528 1.0000
14.000 0.9668 0.08041 0.07178 -0.0168 0.1364 1.0000
14.250 0.9700 0.08359 0.07489 -0.0175 0.1229 1.0000
14.500 0.9750 0.08662 0.07790 -0.0183 0.1114 1.0000
14.750 0.9813 0.08948 0.08074 -0.0190 0.1019 1.0000
15.000 0.9892 0.09205 0.08320 -0.0197 0.0947 1.0000
15.250 1.0011 0.09428 0.08556 -0.0201 0.0882 1.0000
15.500 1.0146 0.09604 0.08718 -0.0204 0.0830 1.0000
15.750 1.0267 0.09845 0.08987 -0.0210 0.0781 1.0000
16.000 1.0399 0.10053 0.09203 -0.0216 0.0740 1.0000
16.250 1.0604 0.10158 0.09303 -0.0215 0.0707 1.0000
16.500 1.0708 0.10448 0.09628 -0.0223 0.0684 1.0000
16.750 1.0783 0.10773 0.09979 -0.0234 0.0662 1.0000
17.000 1.0840 0.11116 0.10342 -0.0247 0.0642 1.0000
17.250 1.0910 0.11426 0.10666 -0.0260 0.0623 1.0000
17.500 1.1030 0.11665 0.10905 -0.0269 0.0604 1.0000
17.750 1.0901 0.12310 0.11586 -0.0302 0.0597 1.0000
18.000 1.0737 0.13043 0.12350 -0.0342 0.0592 1.0000
18.250 1.0523 0.13907 0.13244 -0.0393 0.0590 1.0000
18.500 1.0235 0.14999 0.14361 -0.0462 0.0590 1.0000
18.750 0.9856 0.16451 0.15834 -0.0555 0.0593 1.0000
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