WORTMANN FX 77-080 (fx77080-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 77-080 (fx77080-il) Reynolds number: 1,000,000 Max Cl/Cd: 71.18 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx77080-il-1000000.txt Download as CSV file: xf-fx77080-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 77-080
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.250 -0.9170 0.12492 0.12314 0.0237 1.0000 0.0085
-15.000 -0.9300 0.11724 0.11541 0.0199 1.0000 0.0084
-14.750 -0.9562 0.10702 0.10513 0.0146 1.0000 0.0083
-14.500 -0.9917 0.09518 0.09321 0.0082 1.0000 0.0083
-14.250 -1.0996 0.06881 0.06656 -0.0082 1.0000 0.0077
-14.000 -1.1017 0.06318 0.06085 -0.0124 1.0000 0.0078
-13.750 -1.1292 0.05203 0.04947 -0.0222 1.0000 0.0079
-13.500 -1.1580 0.04333 0.04051 -0.0292 1.0000 0.0078
-13.250 -1.1682 0.03931 0.03631 -0.0309 1.0000 0.0078
-13.000 -1.1708 0.03682 0.03369 -0.0307 1.0000 0.0079
-12.750 -1.1778 0.03430 0.03098 -0.0290 1.0000 0.0080
-12.500 -1.1819 0.03223 0.02875 -0.0263 1.0000 0.0080
-12.250 -1.1702 0.03123 0.02763 -0.0248 1.0000 0.0082
-12.000 -1.1620 0.02962 0.02586 -0.0231 1.0000 0.0082
-11.750 -1.1575 0.02740 0.02342 -0.0210 1.0000 0.0084
-11.500 -1.1575 0.02443 0.02015 -0.0183 1.0000 0.0087
-11.250 -1.1437 0.02308 0.01868 -0.0168 1.0000 0.0091
-11.000 -1.1266 0.02207 0.01757 -0.0155 1.0000 0.0093
-10.750 -1.1076 0.02127 0.01669 -0.0144 1.0000 0.0095
-10.500 -1.0888 0.02039 0.01571 -0.0132 1.0000 0.0097
-10.250 -1.0701 0.01947 0.01468 -0.0120 1.0000 0.0100
-10.000 -1.0506 0.01861 0.01373 -0.0108 1.0000 0.0103
-9.750 -1.0305 0.01783 0.01285 -0.0097 1.0000 0.0105
-9.500 -1.0098 0.01712 0.01204 -0.0086 1.0000 0.0109
-9.250 -0.9889 0.01643 0.01126 -0.0074 1.0000 0.0112
-9.000 -0.9666 0.01594 0.01069 -0.0065 1.0000 0.0115
-8.750 -0.9506 0.01459 0.00919 -0.0046 1.0000 0.0124
-8.500 -0.9291 0.01400 0.00855 -0.0035 1.0000 0.0129
-8.250 -0.9068 0.01353 0.00806 -0.0025 1.0000 0.0136
-8.000 -0.8835 0.01321 0.00771 -0.0016 1.0000 0.0147
-7.750 -0.8609 0.01281 0.00725 -0.0006 1.0000 0.0153
-7.500 -0.8387 0.01240 0.00678 0.0006 1.0000 0.0159
-7.250 -0.8189 0.01167 0.00600 0.0021 1.0000 0.0177
-7.000 -0.7963 0.01135 0.00567 0.0032 1.0000 0.0189
-6.750 -0.7737 0.01105 0.00534 0.0043 1.0000 0.0203
-6.500 -0.7506 0.01082 0.00508 0.0053 1.0000 0.0211
-6.250 -0.7304 0.01025 0.00447 0.0069 1.0000 0.0242
-6.000 -0.7082 0.00998 0.00419 0.0081 1.0000 0.0264
-5.750 -0.6855 0.00978 0.00398 0.0092 1.0000 0.0280
-5.500 -0.6647 0.00938 0.00359 0.0106 1.0000 0.0336
-5.250 -0.6425 0.00918 0.00337 0.0119 1.0000 0.0366
-5.000 -0.6214 0.00885 0.00308 0.0133 1.0000 0.0444
-4.750 -0.6002 0.00857 0.00285 0.0147 1.0000 0.0553
-4.500 -0.5791 0.00830 0.00266 0.0160 1.0000 0.0715
-4.250 -0.5480 0.00802 0.00249 0.0152 0.9988 0.0933
-4.000 -0.5130 0.00782 0.00236 0.0136 0.9967 0.1112
-3.750 -0.4774 0.00762 0.00222 0.0119 0.9942 0.1265
-3.500 -0.4406 0.00741 0.00208 0.0099 0.9916 0.1431
-3.250 -0.4045 0.00722 0.00195 0.0081 0.9895 0.1589
-3.000 -0.3715 0.00701 0.00182 0.0070 0.9862 0.1766
-2.750 -0.3356 0.00678 0.00168 0.0052 0.9836 0.2007
-2.500 -0.3020 0.00649 0.00155 0.0040 0.9796 0.2401
-2.250 -0.2679 0.00613 0.00141 0.0025 0.9747 0.2947
-2.000 -0.2348 0.00580 0.00130 0.0014 0.9695 0.3521
-1.750 -0.1987 0.00546 0.00119 -0.0005 0.9626 0.4168
-1.500 -0.1624 0.00512 0.00109 -0.0024 0.9511 0.4844
-1.250 -0.1258 0.00483 0.00100 -0.0042 0.9347 0.5494
-1.000 -0.0956 0.00462 0.00094 -0.0046 0.9192 0.6048
-0.750 -0.0682 0.00444 0.00090 -0.0043 0.8972 0.6601
-0.500 -0.0443 0.00428 0.00086 -0.0032 0.8721 0.7173
-0.250 -0.0217 0.00420 0.00084 -0.0017 0.8393 0.7625
0.000 -0.0002 0.00417 0.00083 0.0001 0.8017 0.8042
0.250 0.0214 0.00419 0.00084 0.0018 0.7613 0.8433
0.500 0.0443 0.00428 0.00086 0.0032 0.7171 0.8721
0.750 0.0688 0.00442 0.00090 0.0042 0.6659 0.8961
1.000 0.0948 0.00461 0.00094 0.0048 0.6089 0.9169
1.250 0.1260 0.00484 0.00100 0.0042 0.5492 0.9348
1.500 0.1620 0.00514 0.00109 0.0024 0.4817 0.9510
1.750 0.1999 0.00547 0.00120 0.0002 0.4156 0.9631
2.000 0.2350 0.00579 0.00131 -0.0014 0.3530 0.9700
2.250 0.2681 0.00613 0.00142 -0.0026 0.2943 0.9748
2.500 0.3020 0.00648 0.00155 -0.0039 0.2410 0.9796
2.750 0.3356 0.00679 0.00169 -0.0052 0.2003 0.9836
3.000 0.3715 0.00702 0.00182 -0.0070 0.1758 0.9862
3.250 0.4046 0.00723 0.00195 -0.0081 0.1581 0.9897
3.500 0.4404 0.00742 0.00208 -0.0098 0.1424 0.9916
3.750 0.4770 0.00761 0.00222 -0.0118 0.1285 0.9940
4.000 0.5129 0.00781 0.00236 -0.0135 0.1124 0.9967
4.250 0.5482 0.00801 0.00249 -0.0152 0.0948 0.9988
4.500 0.5792 0.00829 0.00266 -0.0160 0.0726 1.0000
4.750 0.6003 0.00856 0.00285 -0.0147 0.0563 1.0000
5.000 0.6215 0.00884 0.00308 -0.0133 0.0449 1.0000
5.250 0.6426 0.00917 0.00336 -0.0119 0.0366 1.0000
5.500 0.6646 0.00938 0.00359 -0.0106 0.0333 1.0000
5.750 0.6853 0.00981 0.00401 -0.0091 0.0282 1.0000
6.000 0.7081 0.00999 0.00421 -0.0080 0.0266 1.0000
6.250 0.7303 0.01026 0.00449 -0.0069 0.0242 1.0000
6.500 0.7508 0.01080 0.00505 -0.0053 0.0210 1.0000
6.750 0.7738 0.01102 0.00531 -0.0043 0.0201 1.0000
7.000 0.7964 0.01133 0.00564 -0.0032 0.0187 1.0000
7.250 0.8187 0.01169 0.00601 -0.0021 0.0175 1.0000
7.500 0.8375 0.01254 0.00695 -0.0004 0.0157 1.0000
7.750 0.8607 0.01284 0.00728 0.0006 0.0153 1.0000
8.000 0.8837 0.01319 0.00768 0.0016 0.0144 1.0000
8.250 0.9063 0.01360 0.00814 0.0026 0.0137 1.0000
8.500 0.9293 0.01397 0.00852 0.0034 0.0129 1.0000
8.750 0.9500 0.01466 0.00927 0.0046 0.0122 1.0000
9.000 0.9667 0.01593 0.01068 0.0065 0.0115 1.0000
9.250 0.9886 0.01648 0.01131 0.0075 0.0112 1.0000
9.500 1.0106 0.01702 0.01194 0.0084 0.0108 1.0000
9.750 1.0309 0.01779 0.01280 0.0096 0.0106 1.0000
10.000 1.0506 0.01863 0.01375 0.0108 0.0103 1.0000
10.250 1.0709 0.01936 0.01457 0.0119 0.0099 1.0000
10.500 1.0901 0.02023 0.01553 0.0131 0.0097 1.0000
10.750 1.1086 0.02115 0.01655 0.0143 0.0095 1.0000
11.000 1.1281 0.02189 0.01735 0.0153 0.0092 1.0000
11.250 1.1442 0.02302 0.01860 0.0166 0.0089 1.0000
11.500 1.1571 0.02454 0.02027 0.0183 0.0088 1.0000
11.750 1.1550 0.02777 0.02382 0.0212 0.0084 1.0000
12.000 1.1526 0.03078 0.02711 0.0238 0.0083 1.0000
12.250 1.1620 0.03221 0.02869 0.0253 0.0082 1.0000
12.500 1.1693 0.03338 0.02998 0.0273 0.0081 1.0000
12.750 1.1780 0.03438 0.03108 0.0289 0.0079 1.0000
13.000 1.1643 0.03757 0.03447 0.0306 0.0080 1.0000
13.250 1.1504 0.04150 0.03861 0.0301 0.0080 1.0000
13.500 1.1588 0.04343 0.04062 0.0289 0.0076 1.0000
13.750 1.1202 0.05411 0.05159 0.0201 0.0080 1.0000
14.000 1.0389 0.07661 0.07447 0.0026 0.0082 1.0000
14.250 1.0411 0.08120 0.07910 -0.0003 0.0081 1.0000
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