WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=100,000 Ncrit=5
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Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il) Reynolds number: 100,000 Max Cl/Cd: 29.24 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05191-il-100000-n5.txt Download as CSV file: xf-fx05191-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-191 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-14.250 -0.4619 0.09360 0.08805 -0.1019 0.9726 0.0357
-14.000 -0.4884 0.08517 0.07943 -0.1076 0.9686 0.0355
-13.750 -0.5135 0.07798 0.07203 -0.1124 0.9646 0.0354
-13.500 -0.5321 0.07202 0.06582 -0.1164 0.9614 0.0353
-13.250 -0.5477 0.06677 0.06030 -0.1197 0.9588 0.0353
-13.000 -0.5639 0.06275 0.05603 -0.1207 0.9541 0.0353
-12.750 -0.5764 0.05884 0.05180 -0.1219 0.9504 0.0354
-12.500 -0.5832 0.05532 0.04794 -0.1229 0.9475 0.0355
-12.250 -0.5875 0.05249 0.04479 -0.1228 0.9439 0.0357
-12.000 -0.5860 0.05034 0.04250 -0.1219 0.9392 0.0360
-11.750 -0.5759 0.04843 0.04046 -0.1221 0.9360 0.0366
-11.500 -0.5639 0.04670 0.03858 -0.1224 0.9336 0.0374
-11.250 -0.5535 0.04522 0.03696 -0.1221 0.9308 0.0383
-11.000 -0.5542 0.04407 0.03566 -0.1192 0.9252 0.0388
-10.750 -0.5432 0.04258 0.03395 -0.1184 0.9217 0.0398
-10.500 -0.5237 0.04087 0.03198 -0.1186 0.9195 0.0406
-10.250 -0.4970 0.03914 0.02997 -0.1195 0.9180 0.0415
-10.000 -0.4897 0.03838 0.02905 -0.1165 0.9126 0.0420
-9.750 -0.4637 0.03715 0.02769 -0.1166 0.9096 0.0430
-9.500 -0.4347 0.03606 0.02662 -0.1175 0.9072 0.0445
-9.250 -0.4064 0.03509 0.02560 -0.1184 0.9050 0.0464
-9.000 -0.3749 0.03413 0.02454 -0.1196 0.9033 0.0488
-8.750 -0.3685 0.03385 0.02419 -0.1163 0.8976 0.0501
-8.500 -0.3489 0.03320 0.02353 -0.1152 0.8939 0.0517
-8.250 -0.3278 0.03243 0.02278 -0.1149 0.8910 0.0537
-8.000 -0.3046 0.03165 0.02197 -0.1151 0.8886 0.0564
-7.750 -0.3059 0.03148 0.02177 -0.1108 0.8824 0.0586
-7.500 -0.2992 0.03101 0.02128 -0.1080 0.8773 0.0617
-7.250 -0.2846 0.03027 0.02053 -0.1069 0.8739 0.0660
-7.000 -0.2833 0.02993 0.02014 -0.1032 0.8685 0.0697
-6.750 -0.2901 0.02971 0.01988 -0.0980 0.8612 0.0726
-6.500 -0.2804 0.02894 0.01912 -0.0959 0.8575 0.0793
-6.250 -0.2988 0.02901 0.01915 -0.0885 0.8485 0.0824
-6.000 -0.2924 0.02832 0.01852 -0.0858 0.8434 0.0943
-5.750 -0.2774 0.02732 0.01768 -0.0848 0.8404 0.1234
-5.500 -0.2980 0.02730 0.01776 -0.0769 0.8298 0.1396
-5.250 -0.2939 0.02571 0.01679 -0.0746 0.8256 0.2449
-5.000 -0.3096 0.02488 0.01659 -0.0683 0.8167 0.3525
-4.750 -0.2987 0.02435 0.01669 -0.0656 0.8115 0.4888
-4.500 -0.2709 0.02433 0.01684 -0.0652 0.8089 0.5550
-4.250 -0.2382 0.02478 0.01735 -0.0649 0.8071 0.5988
-4.000 -0.2464 0.02536 0.01798 -0.0585 0.7961 0.6195
-3.750 -0.2181 0.02648 0.01910 -0.0565 0.7933 0.6470
-3.500 -0.1847 0.02738 0.01991 -0.0558 0.7913 0.6635
-3.000 -0.1612 0.02789 0.02026 -0.0502 0.7775 0.6781
-2.750 -0.1290 0.02740 0.01960 -0.0518 0.7754 0.6873
-2.500 -0.1286 0.02800 0.02018 -0.0470 0.7655 0.6908
-2.250 -0.1021 0.02801 0.02009 -0.0467 0.7618 0.6955
-2.000 -0.0696 0.02757 0.01950 -0.0483 0.7596 0.7038
-1.500 -0.0413 0.02815 0.01998 -0.0438 0.7463 0.7128
-1.250 -0.0085 0.02777 0.01947 -0.0453 0.7441 0.7202
-1.000 -0.0036 0.02836 0.02005 -0.0416 0.7348 0.7243
-0.750 0.0221 0.02831 0.01994 -0.0414 0.7311 0.7299
-0.500 0.0545 0.02799 0.01952 -0.0427 0.7289 0.7366
-0.250 0.0613 0.02858 0.02011 -0.0395 0.7202 0.7409
0.000 0.0868 0.02853 0.01999 -0.0394 0.7162 0.7467
0.250 0.1191 0.02824 0.01962 -0.0406 0.7139 0.7530
0.500 0.1488 0.02805 0.01939 -0.0406 0.7123 0.7565
0.750 0.1522 0.02882 0.02016 -0.0376 0.7016 0.7630
1.000 0.1843 0.02855 0.01984 -0.0388 0.6992 0.7692
1.250 0.2133 0.02830 0.01956 -0.0386 0.6975 0.7726
1.750 0.2505 0.02892 0.02015 -0.0374 0.6849 0.7849
2.000 0.2777 0.02868 0.01990 -0.0368 0.6830 0.7883
2.250 0.3090 0.02834 0.01954 -0.0372 0.6815 0.7927
2.500 0.3162 0.02934 0.02055 -0.0357 0.6709 0.7998
2.750 0.3430 0.02913 0.02035 -0.0354 0.6686 0.8035
3.000 0.3727 0.02882 0.02004 -0.0354 0.6669 0.8075
3.500 0.4087 0.02967 0.02093 -0.0340 0.6544 0.8181
3.750 0.4362 0.02942 0.02071 -0.0337 0.6523 0.8218
4.000 0.4691 0.02905 0.02035 -0.0345 0.6507 0.8261
4.500 0.4992 0.03015 0.02154 -0.0322 0.6376 0.8357
4.750 0.5302 0.02981 0.02124 -0.0325 0.6357 0.8397
5.000 0.5661 0.02939 0.02086 -0.0338 0.6342 0.8440
5.500 0.5901 0.03071 0.02231 -0.0305 0.6204 0.8529
5.750 0.6241 0.03027 0.02193 -0.0313 0.6186 0.8569
6.000 0.6632 0.02975 0.02147 -0.0331 0.6172 0.8608
6.500 0.6821 0.03122 0.02310 -0.0291 0.6026 0.8692
6.750 0.7197 0.03062 0.02258 -0.0303 0.6010 0.8728
7.250 0.7443 0.03216 0.02430 -0.0277 0.5863 0.8808
7.500 0.7656 0.03233 0.02458 -0.0270 0.5814 0.8845
7.750 0.7725 0.03342 0.02577 -0.0253 0.5719 0.8887
8.000 0.8237 0.03171 0.02415 -0.0275 0.5689 0.8915
8.250 0.8253 0.03284 0.02536 -0.0250 0.5563 0.8954
8.500 0.8552 0.03190 0.02451 -0.0247 0.5464 0.8987
8.750 0.8939 0.03057 0.02322 -0.0253 0.5357 0.9017
9.000 0.8993 0.03149 0.02423 -0.0232 0.5217 0.9058
9.250 0.9103 0.03217 0.02501 -0.0218 0.5080 0.9095
9.500 0.9217 0.03261 0.02554 -0.0201 0.4939 0.9130
9.750 0.9360 0.03306 0.02607 -0.0189 0.4799 0.9167
10.000 0.9503 0.03366 0.02676 -0.0180 0.4650 0.9205
10.250 0.9600 0.03451 0.02770 -0.0166 0.4481 0.9240
10.500 0.9678 0.03540 0.02867 -0.0150 0.4279 0.9277
10.750 0.9800 0.03607 0.02934 -0.0138 0.4033 0.9317
11.000 0.9896 0.03699 0.03019 -0.0125 0.3696 0.9356
11.250 0.9950 0.03797 0.03095 -0.0105 0.3264 0.9396
11.500 0.9927 0.03988 0.03258 -0.0085 0.2798 0.9435
11.750 0.9857 0.04243 0.03486 -0.0067 0.2360 0.9477
12.000 0.9775 0.04517 0.03740 -0.0050 0.2006 0.9527
12.250 0.9727 0.04791 0.03998 -0.0040 0.1707 0.9583
12.500 0.9722 0.05049 0.04245 -0.0035 0.1472 0.9648
13.000 0.9769 0.05513 0.04701 -0.0033 0.1169 1.0000
13.250 0.9838 0.05752 0.04938 -0.0037 0.1071 1.0000
13.500 0.9902 0.05999 0.05181 -0.0041 0.0991 1.0000
13.750 1.0003 0.06210 0.05400 -0.0046 0.0924 1.0000
14.000 1.0077 0.06449 0.05638 -0.0050 0.0867 1.0000
14.250 1.0189 0.06650 0.05846 -0.0055 0.0817 1.0000
14.500 1.0292 0.06865 0.06067 -0.0061 0.0767 1.0000
14.750 1.0388 0.07078 0.06275 -0.0065 0.0726 1.0000
15.000 1.0519 0.07267 0.06481 -0.0071 0.0684 1.0000
15.250 1.0629 0.07477 0.06696 -0.0077 0.0646 1.0000
15.500 1.0743 0.07674 0.06889 -0.0081 0.0615 1.0000
15.750 1.0867 0.07880 0.07115 -0.0088 0.0582 1.0000
16.000 1.0984 0.08091 0.07335 -0.0094 0.0554 1.0000
16.250 1.1090 0.08311 0.07558 -0.0102 0.0531 1.0000
16.500 1.1205 0.08524 0.07780 -0.0108 0.0509 1.0000
16.750 1.1299 0.08774 0.08051 -0.0117 0.0485 1.0000
17.000 1.1381 0.09036 0.08324 -0.0127 0.0465 1.0000
17.250 1.1465 0.09291 0.08585 -0.0137 0.0448 1.0000
17.500 1.1556 0.09535 0.08831 -0.0147 0.0433 1.0000
17.750 1.1595 0.09872 0.09196 -0.0159 0.0417 1.0000
18.000 1.1629 0.10212 0.09557 -0.0173 0.0401 1.0000
18.250 1.1659 0.10554 0.09915 -0.0189 0.0388 1.0000
18.500 1.1698 0.10881 0.10251 -0.0205 0.0377 1.0000
18.750 1.1762 0.11163 0.10535 -0.0220 0.0367 1.0000
19.000 1.1730 0.11619 0.11015 -0.0242 0.0357 1.0000
19.250 1.1659 0.12149 0.11575 -0.0269 0.0348 1.0000
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