WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=100,000 Ncrit=0
| Details | Polar file |
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Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il) Reynolds number: 100,000 Max Cl/Cd: 23.37 at α=11.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx3-il-100000.txt Download as CSV file: xf-fx3-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 3 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.250 -0.5325 0.13449 0.13073 -0.0316 1.0001 0.1634
-10.000 -0.4936 0.13358 0.12976 -0.0269 1.0001 0.1683
-9.750 -0.5027 0.13060 0.12679 -0.0267 1.0001 0.1766
-9.500 -0.5161 0.12652 0.12274 -0.0266 1.0001 0.1839
-9.250 -0.5262 0.12341 0.11965 -0.0262 1.0001 0.1933
-9.000 -0.5223 0.12108 0.11732 -0.0243 1.0001 0.2032
-8.250 -0.9545 0.07064 0.06431 -0.0259 1.0001 0.0692
-8.000 -0.9497 0.06567 0.05907 -0.0247 1.0001 0.0681
-7.750 -0.9419 0.06179 0.05476 -0.0236 1.0001 0.0684
-7.500 -0.9298 0.05878 0.05121 -0.0228 1.0001 0.0695
-7.250 -0.9146 0.05585 0.04777 -0.0222 1.0001 0.0705
-7.000 -0.8986 0.05134 0.04295 -0.0215 1.0001 0.0717
-6.750 -0.8811 0.04919 0.04081 -0.0210 1.0001 0.0751
-6.500 -0.8617 0.04760 0.03902 -0.0204 1.0001 0.0791
-6.250 -0.8406 0.04590 0.03693 -0.0196 1.0001 0.0826
-6.000 -0.8201 0.04407 0.03481 -0.0188 1.0001 0.0872
-5.750 -0.8009 0.04280 0.03357 -0.0178 1.0001 0.0927
-5.500 -0.7799 0.04193 0.03249 -0.0169 1.0001 0.0989
-5.250 -0.7607 0.04083 0.03142 -0.0155 1.0000 0.1052
-5.000 -0.7356 0.04049 0.03101 -0.0154 0.9985 0.1131
-4.750 -0.7122 0.04013 0.03070 -0.0146 0.9970 0.1207
-4.500 -0.6859 0.04022 0.03077 -0.0147 0.9953 0.1300
-4.250 -0.6638 0.04022 0.03093 -0.0138 0.9940 0.1380
-4.000 -0.6416 0.04005 0.03074 -0.0132 0.9910 0.1478
-3.750 -0.6185 0.04011 0.03099 -0.0127 0.9883 0.1593
-3.500 -0.5919 0.04046 0.03148 -0.0131 0.9860 0.1769
-3.250 -0.5599 0.03889 0.03216 -0.0172 0.9858 0.4411
-3.000 -0.5553 0.04561 0.03944 -0.0055 0.9771 0.6770
-2.750 -0.5429 0.04932 0.04300 0.0018 0.9725 0.7073
-2.500 -0.5399 0.05166 0.04530 0.0108 0.9690 0.7258
-2.250 -0.1639 0.06728 0.06017 -0.0250 1.0001 0.9999
-2.000 -0.1564 0.06685 0.05966 -0.0236 1.0001 0.9999
-1.750 -0.1488 0.06648 0.05922 -0.0221 1.0001 0.9999
-1.500 -0.1412 0.06616 0.05884 -0.0205 1.0001 0.9999
-1.250 -0.1161 0.06562 0.05822 -0.0226 0.9961 0.9999
-1.000 -0.0837 0.06524 0.05776 -0.0260 0.9877 0.9999
-0.750 -0.0594 0.06524 0.05768 -0.0278 0.9813 0.9999
-0.500 -0.0330 0.06520 0.05758 -0.0299 0.9729 0.9999
-0.250 -0.0162 0.06497 0.05730 -0.0300 0.9648 0.9999
0.000 0.0087 0.06531 0.05758 -0.0318 0.9581 0.9999
0.250 0.0214 0.06507 0.05731 -0.0310 0.9496 0.9999
0.500 0.0453 0.06550 0.05770 -0.0324 0.9432 0.9999
0.750 0.0551 0.06534 0.05752 -0.0310 0.9350 0.9999
1.000 0.0780 0.06578 0.05792 -0.0322 0.9284 0.9999
1.250 0.0866 0.06578 0.05792 -0.0306 0.9208 0.9999
1.500 0.1080 0.06615 0.05826 -0.0313 0.9135 0.9999
1.750 0.1347 0.06781 0.05989 -0.0332 0.9103 0.9999
2.000 0.1359 0.06662 0.05872 -0.0300 0.8984 0.9999
2.250 -0.0581 0.06325 0.05527 0.0131 0.8804 0.9482
2.500 -0.0744 0.06198 0.05400 0.0194 0.8703 0.9436
2.750 -0.1177 0.06160 0.05355 0.0320 0.8640 0.9349
3.000 -0.1308 0.05977 0.05173 0.0375 0.8533 0.9326
3.250 -0.1010 0.06106 0.05298 0.0355 0.8493 0.9321
3.500 -0.1089 0.05992 0.05185 0.0397 0.8399 0.9308
3.750 -0.0771 0.06105 0.05295 0.0373 0.8350 0.9297
4.000 -0.0763 0.06059 0.05251 0.0396 0.8264 0.9282
4.250 -0.0412 0.06170 0.05360 0.0367 0.8206 0.9280
4.500 -0.0347 0.06162 0.05355 0.0379 0.8120 0.9272
4.750 0.0083 0.06300 0.05493 0.0337 0.8056 0.9264
5.000 0.0215 0.06286 0.05482 0.0338 0.7944 0.9253
5.250 0.0589 0.06236 0.05431 0.0315 0.7732 0.9250
5.500 0.0971 0.06212 0.05408 0.0289 0.7588 0.9249
5.750 0.1294 0.06217 0.05417 0.0266 0.7477 0.9243
6.000 0.1614 0.06238 0.05442 0.0242 0.7376 0.9234
6.250 0.1965 0.06259 0.05468 0.0215 0.7292 0.9230
6.500 0.2310 0.06269 0.05484 0.0191 0.7211 0.9228
6.750 0.2553 0.06290 0.05513 0.0179 0.7107 0.9223
7.000 0.2883 0.06301 0.05531 0.0156 0.7023 0.9216
7.250 0.3242 0.06302 0.05542 0.0131 0.6944 0.9208
7.500 0.3492 0.06333 0.05581 0.0118 0.6838 0.9200
7.750 0.3947 0.06302 0.05562 0.0083 0.6783 0.9198
8.000 0.4159 0.06344 0.05614 0.0075 0.6666 0.9194
8.250 0.4657 0.06280 0.05563 0.0038 0.6622 0.9191
8.500 0.4866 0.06319 0.05615 0.0031 0.6494 0.9182
8.750 0.5280 0.06261 0.05571 0.0004 0.6423 0.9174
9.000 0.5663 0.06171 0.05497 -0.0015 0.6318 0.9167
9.250 0.6050 0.06026 0.05367 -0.0030 0.6189 0.9160
9.500 0.6783 0.05564 0.04927 -0.0067 0.6138 0.9156
9.750 0.7115 0.05442 0.04823 -0.0075 0.6004 0.9148
10.000 0.7726 0.05082 0.04486 -0.0105 0.5971 0.9145
10.250 0.8043 0.04962 0.04388 -0.0110 0.5833 0.9141
10.500 0.8447 0.04761 0.04208 -0.0121 0.5698 0.9140
10.750 0.8914 0.04511 0.03980 -0.0136 0.5528 0.9138
11.000 0.9362 0.04268 0.03748 -0.0147 0.5177 0.9133
11.250 0.9681 0.04142 0.03596 -0.0146 0.4487 0.9127
11.500 0.9761 0.04242 0.03643 -0.0126 0.3595 0.9118
11.750 0.9720 0.04474 0.03814 -0.0100 0.2787 0.9109
12.000 0.9688 0.04733 0.04024 -0.0081 0.2224 0.9100
12.250 0.9715 0.04967 0.04228 -0.0069 0.1830 0.9092
12.500 0.9751 0.05180 0.04420 -0.0056 0.1538 0.9086
12.750 0.9780 0.05400 0.04617 -0.0042 0.1278 0.9080
13.000 0.9820 0.05622 0.04822 -0.0029 0.1042 0.9075
13.250 0.9950 0.05785 0.04965 -0.0020 0.0869 0.9070
13.500 1.0114 0.05932 0.05112 -0.0017 0.0762 0.9066
13.750 1.0371 0.06040 0.05227 -0.0019 0.0682 0.9063
14.000 1.0763 0.06119 0.05285 -0.0033 0.0615 0.9062
14.250 1.0933 0.06294 0.05492 -0.0032 0.0579 0.9058
14.500 1.1172 0.06460 0.05675 -0.0037 0.0546 0.9055
14.750 1.1652 0.06663 0.05871 -0.0063 0.0512 0.9056
15.000 1.1686 0.06934 0.06184 -0.0051 0.0501 0.9053
15.250 1.1708 0.07236 0.06525 -0.0040 0.0488 0.9050
15.500 1.1712 0.07564 0.06888 -0.0030 0.0477 0.9048
15.750 1.1681 0.07932 0.07290 -0.0020 0.0472 0.9045
16.000 1.1598 0.08344 0.07738 -0.0009 0.0469 0.9041
16.250 1.1463 0.08802 0.08232 0.0000 0.0469 0.9036
16.500 1.1290 0.09309 0.08773 0.0005 0.0471 0.9031
16.750 1.1081 0.09872 0.09370 0.0003 0.0474 0.9024
17.000 1.0845 0.10493 0.10023 -0.0006 0.0477 0.9017
17.250 1.0591 0.11185 0.10744 -0.0027 0.0482 0.9009
17.500 1.0323 0.11955 0.11541 -0.0059 0.0487 0.9001
17.750 1.0053 0.12807 0.12417 -0.0104 0.0494 0.8994
18.000 0.9799 0.13721 0.13349 -0.0160 0.0500 0.8986
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