Falcon (falcon-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Falcon (falcon-il) Reynolds number: 1,000,000 Max Cl/Cd: 92.37 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-falcon-il-1000000-n5.txt Download as CSV file: xf-falcon-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Falcon
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.9737 0.12941 0.12703 -0.0029 1.0000 0.0091
-18.250 -1.1019 0.10093 0.09822 -0.0185 1.0000 0.0088
-18.000 -1.2000 0.07813 0.07503 -0.0312 1.0000 0.0085
-17.750 -1.2423 0.06702 0.06369 -0.0378 1.0000 0.0085
-17.500 -1.2687 0.05917 0.05566 -0.0423 1.0000 0.0084
-17.250 -1.2878 0.05299 0.04932 -0.0456 1.0000 0.0085
-17.000 -1.3012 0.04801 0.04420 -0.0477 1.0000 0.0085
-16.750 -1.3105 0.04397 0.04003 -0.0489 1.0000 0.0086
-16.500 -1.3160 0.04069 0.03663 -0.0494 1.0000 0.0087
-16.250 -1.3192 0.03790 0.03374 -0.0493 1.0000 0.0088
-16.000 -1.3198 0.03556 0.03130 -0.0488 1.0000 0.0089
-15.750 -1.3181 0.03359 0.02924 -0.0478 1.0000 0.0090
-15.500 -1.3152 0.03185 0.02742 -0.0466 1.0000 0.0091
-15.250 -1.3108 0.03035 0.02582 -0.0451 1.0000 0.0092
-15.000 -1.3051 0.02903 0.02443 -0.0434 1.0000 0.0094
-14.750 -1.2990 0.02783 0.02315 -0.0415 1.0000 0.0095
-14.500 -1.2920 0.02676 0.02200 -0.0394 1.0000 0.0096
-14.250 -1.2841 0.02583 0.02100 -0.0371 1.0000 0.0098
-14.000 -1.2764 0.02496 0.02005 -0.0345 1.0000 0.0099
-13.750 -1.2682 0.02419 0.01921 -0.0317 1.0000 0.0101
-13.500 -1.2603 0.02348 0.01843 -0.0287 1.0000 0.0102
-13.250 -1.2503 0.02282 0.01770 -0.0259 1.0000 0.0104
-13.000 -1.2363 0.02214 0.01695 -0.0238 1.0000 0.0105
-12.750 -1.2208 0.02150 0.01625 -0.0220 1.0000 0.0107
-12.500 -1.2045 0.02091 0.01559 -0.0203 1.0000 0.0108
-12.250 -1.1897 0.02015 0.01478 -0.0183 1.0000 0.0111
-12.000 -1.1728 0.01952 0.01410 -0.0166 1.0000 0.0114
-11.750 -1.1545 0.01896 0.01351 -0.0151 1.0000 0.0117
-11.500 -1.1353 0.01846 0.01297 -0.0137 1.0000 0.0120
-11.250 -1.1157 0.01798 0.01245 -0.0124 1.0000 0.0123
-11.000 -1.0957 0.01752 0.01196 -0.0111 1.0000 0.0126
-10.750 -1.0754 0.01707 0.01147 -0.0098 1.0000 0.0130
-10.500 -1.0550 0.01664 0.01099 -0.0085 1.0000 0.0133
-10.250 -1.0344 0.01623 0.01054 -0.0072 1.0000 0.0135
-10.000 -1.0056 0.01575 0.01001 -0.0077 0.9990 0.0138
-9.750 -0.9877 0.01520 0.00944 -0.0059 0.9759 0.0143
-9.500 -0.9539 0.01470 0.00892 -0.0074 0.9698 0.0149
-9.250 -0.9183 0.01423 0.00843 -0.0094 0.9655 0.0154
-9.000 -0.8807 0.01379 0.00795 -0.0118 0.9619 0.0160
-8.750 -0.8408 0.01337 0.00750 -0.0147 0.9584 0.0167
-8.250 -0.7561 0.01247 0.00655 -0.0217 0.9506 0.0185
-8.000 -0.7146 0.01208 0.00613 -0.0250 0.9440 0.0195
-7.750 -0.6790 0.01178 0.00578 -0.0269 0.9348 0.0204
-7.500 -0.6474 0.01153 0.00548 -0.0278 0.9244 0.0211
-7.250 -0.6205 0.01125 0.00517 -0.0277 0.9124 0.0226
-7.000 -0.5948 0.01101 0.00491 -0.0273 0.8999 0.0240
-6.750 -0.5692 0.01082 0.00466 -0.0268 0.8861 0.0253
-6.500 -0.5443 0.01062 0.00441 -0.0261 0.8696 0.0268
-6.250 -0.5200 0.01043 0.00417 -0.0253 0.8505 0.0290
-6.000 -0.4957 0.01028 0.00395 -0.0245 0.8293 0.0311
-5.750 -0.4719 0.01012 0.00372 -0.0236 0.8057 0.0342
-5.500 -0.4482 0.01001 0.00352 -0.0227 0.7804 0.0373
-5.250 -0.4244 0.00989 0.00332 -0.0217 0.7543 0.0412
-5.000 -0.4005 0.00979 0.00315 -0.0208 0.7287 0.0455
-4.750 -0.3766 0.00968 0.00298 -0.0199 0.7036 0.0519
-4.500 -0.3524 0.00958 0.00283 -0.0191 0.6812 0.0590
-4.250 -0.3277 0.00949 0.00269 -0.0184 0.6599 0.0661
-4.000 -0.3029 0.00939 0.00256 -0.0177 0.6409 0.0742
-3.750 -0.2778 0.00931 0.00244 -0.0171 0.6234 0.0820
-3.500 -0.2523 0.00924 0.00234 -0.0165 0.6077 0.0899
-3.250 -0.2270 0.00914 0.00223 -0.0159 0.5928 0.1001
-3.000 -0.2013 0.00908 0.00214 -0.0154 0.5790 0.1082
-2.750 -0.1756 0.00901 0.00205 -0.0149 0.5658 0.1178
-2.500 -0.1500 0.00893 0.00197 -0.0144 0.5531 0.1294
-2.250 -0.1243 0.00883 0.00188 -0.0139 0.5413 0.1443
-2.000 -0.0987 0.00874 0.00181 -0.0134 0.5297 0.1616
-1.750 -0.0741 0.00858 0.00172 -0.0127 0.5181 0.1922
-1.500 -0.0557 0.00797 0.00154 -0.0109 0.5074 0.3232
-1.250 -0.0323 0.00774 0.00147 -0.0100 0.4967 0.3812
-1.000 -0.0083 0.00759 0.00142 -0.0091 0.4858 0.4264
-0.750 0.0165 0.00747 0.00138 -0.0084 0.4751 0.4618
-0.500 0.0411 0.00736 0.00136 -0.0077 0.4645 0.5001
-0.250 0.0656 0.00727 0.00134 -0.0069 0.4534 0.5364
0.000 0.0903 0.00720 0.00133 -0.0062 0.4422 0.5704
0.250 0.1145 0.00710 0.00132 -0.0054 0.4316 0.6073
0.500 0.1387 0.00704 0.00133 -0.0045 0.4211 0.6432
0.750 0.1628 0.00699 0.00134 -0.0036 0.4094 0.6778
1.000 0.1869 0.00695 0.00137 -0.0027 0.3979 0.7136
1.250 0.2110 0.00693 0.00141 -0.0018 0.3867 0.7456
1.500 0.2352 0.00693 0.00146 -0.0009 0.3755 0.7749
1.750 0.2599 0.00694 0.00151 -0.0001 0.3648 0.8015
2.000 0.2857 0.00698 0.00156 0.0004 0.3541 0.8183
2.250 0.3120 0.00706 0.00162 0.0008 0.3434 0.8297
2.500 0.3385 0.00711 0.00167 0.0012 0.3340 0.8418
2.750 0.3652 0.00718 0.00174 0.0015 0.3251 0.8535
3.000 0.3918 0.00727 0.00181 0.0018 0.3146 0.8655
3.250 0.4190 0.00733 0.00189 0.0019 0.3062 0.8782
3.500 0.4467 0.00743 0.00198 0.0020 0.2972 0.8909
3.750 0.4759 0.00751 0.00207 0.0017 0.2876 0.9041
4.000 0.5072 0.00762 0.00217 0.0009 0.2779 0.9184
4.250 0.5429 0.00774 0.00229 -0.0010 0.2682 0.9321
4.500 0.5814 0.00788 0.00241 -0.0035 0.2594 0.9427
4.750 0.6250 0.00806 0.00256 -0.0073 0.2486 0.9476
5.250 0.7060 0.00846 0.00288 -0.0134 0.2256 0.9564
5.500 0.7458 0.00868 0.00306 -0.0163 0.2160 0.9592
5.750 0.7844 0.00893 0.00327 -0.0189 0.2057 0.9623
6.000 0.8216 0.00915 0.00347 -0.0211 0.1965 0.9664
6.250 0.8571 0.00940 0.00369 -0.0230 0.1871 0.9703
6.500 0.8904 0.00969 0.00393 -0.0244 0.1749 0.9738
6.750 0.9214 0.01002 0.00418 -0.0254 0.1606 0.9777
7.250 0.9735 0.01064 0.00473 -0.0250 0.1427 0.9973
7.500 1.0048 0.01094 0.00498 -0.0261 0.1342 0.9988
7.750 1.0364 0.01122 0.00524 -0.0272 0.1255 0.9998
8.000 1.0607 0.01150 0.00549 -0.0267 0.1184 1.0000
8.250 1.0819 0.01182 0.00576 -0.0256 0.1095 1.0000
8.500 1.1034 0.01215 0.00605 -0.0245 0.1003 1.0000
8.750 1.1245 0.01251 0.00638 -0.0234 0.0911 1.0000
9.000 1.1439 0.01302 0.00679 -0.0221 0.0761 1.0000
9.250 1.1513 0.01442 0.00788 -0.0189 0.0305 1.0000
9.500 1.1685 0.01508 0.00849 -0.0172 0.0208 1.0000
9.750 1.1880 0.01556 0.00898 -0.0159 0.0174 1.0000
10.000 1.2078 0.01602 0.00944 -0.0147 0.0154 1.0000
10.250 1.2271 0.01649 0.00993 -0.0134 0.0138 1.0000
10.500 1.2461 0.01696 0.01042 -0.0121 0.0127 1.0000
10.750 1.2652 0.01741 0.01091 -0.0108 0.0120 1.0000
11.000 1.2832 0.01791 0.01144 -0.0093 0.0114 1.0000
11.250 1.3002 0.01847 0.01202 -0.0078 0.0107 1.0000
11.500 1.3160 0.01908 0.01266 -0.0061 0.0102 1.0000
11.750 1.3316 0.01962 0.01325 -0.0043 0.0099 1.0000
12.000 1.3427 0.02018 0.01385 -0.0017 0.0096 1.0000
12.250 1.3524 0.02078 0.01450 0.0010 0.0093 1.0000
12.500 1.3624 0.02144 0.01521 0.0035 0.0090 1.0000
12.750 1.3717 0.02222 0.01604 0.0059 0.0088 1.0000
13.000 1.3803 0.02311 0.01698 0.0080 0.0085 1.0000
13.250 1.3878 0.02416 0.01808 0.0100 0.0082 1.0000
13.500 1.3940 0.02538 0.01937 0.0119 0.0079 1.0000
13.750 1.4004 0.02670 0.02075 0.0135 0.0078 1.0000
14.000 1.4075 0.02806 0.02219 0.0147 0.0076 1.0000
14.250 1.4134 0.02963 0.02383 0.0158 0.0075 1.0000
14.500 1.4183 0.03139 0.02568 0.0166 0.0074 1.0000
14.750 1.4218 0.03343 0.02779 0.0172 0.0073 1.0000
15.000 1.4245 0.03569 0.03014 0.0175 0.0072 1.0000
15.250 1.4254 0.03827 0.03282 0.0175 0.0071 1.0000
15.500 1.4249 0.04114 0.03578 0.0172 0.0070 1.0000
15.750 1.4223 0.04439 0.03913 0.0167 0.0069 1.0000
16.000 1.4182 0.04790 0.04273 0.0159 0.0068 1.0000
16.250 1.4122 0.05175 0.04669 0.0150 0.0067 1.0000
16.500 1.4035 0.05601 0.05106 0.0138 0.0067 1.0000
16.750 1.3933 0.06055 0.05570 0.0125 0.0066 1.0000
17.000 1.3803 0.06562 0.06089 0.0109 0.0066 1.0000
17.250 1.3655 0.07104 0.06642 0.0091 0.0066 1.0000
17.500 1.3504 0.07664 0.07214 0.0071 0.0065 1.0000
17.750 1.3335 0.08264 0.07826 0.0049 0.0065 1.0000
18.000 1.3154 0.08892 0.08465 0.0025 0.0065 1.0000
18.250 1.2967 0.09542 0.09127 0.0000 0.0064 1.0000
18.500 1.2787 0.10191 0.09787 -0.0026 0.0064 1.0000
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