GIII BL45 AIRFOIL (giiib-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GIII BL45 AIRFOIL (giiib-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.33 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-giiib-il-1000000-n5.txt Download as CSV file: xf-giiib-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GIII BL45 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-15.500 -0.8804 0.12396 0.12223 0.0157 1.0000 0.0036
-15.250 -1.1149 0.06705 0.06495 -0.0166 1.0000 0.0032
-15.000 -1.1630 0.05279 0.05039 -0.0276 1.0000 0.0031
-14.750 -1.1851 0.04655 0.04395 -0.0306 1.0000 0.0031
-14.500 -1.1998 0.04220 0.03942 -0.0312 1.0000 0.0032
-14.250 -1.2102 0.03883 0.03586 -0.0306 1.0000 0.0032
-14.000 -1.2166 0.03615 0.03302 -0.0292 1.0000 0.0032
-13.750 -1.2196 0.03394 0.03063 -0.0273 1.0000 0.0033
-13.500 -1.2203 0.03203 0.02856 -0.0250 1.0000 0.0033
-13.250 -1.2177 0.03041 0.02679 -0.0226 1.0000 0.0033
-13.000 -1.2131 0.02894 0.02517 -0.0201 1.0000 0.0034
-12.750 -1.2050 0.02762 0.02370 -0.0179 1.0000 0.0034
-12.500 -1.1931 0.02638 0.02232 -0.0162 1.0000 0.0035
-12.250 -1.1792 0.02524 0.02104 -0.0147 1.0000 0.0035
-12.000 -1.1639 0.02418 0.01985 -0.0133 1.0000 0.0035
-11.750 -1.1522 0.02262 0.01811 -0.0115 1.0000 0.0037
-11.500 -1.1362 0.02147 0.01682 -0.0101 1.0000 0.0039
-11.250 -1.1178 0.02056 0.01582 -0.0089 1.0000 0.0040
-11.000 -1.0981 0.01980 0.01495 -0.0079 1.0000 0.0042
-10.750 -1.0775 0.01910 0.01418 -0.0070 1.0000 0.0044
-10.500 -1.0565 0.01846 0.01347 -0.0062 1.0000 0.0045
-10.250 -1.0352 0.01784 0.01277 -0.0053 1.0000 0.0047
-10.000 -1.0137 0.01724 0.01210 -0.0045 1.0000 0.0049
-9.750 -0.9920 0.01666 0.01144 -0.0036 1.0000 0.0052
-9.500 -0.9702 0.01611 0.01083 -0.0027 1.0000 0.0054
-9.250 -0.9482 0.01560 0.01025 -0.0018 1.0000 0.0056
-9.000 -0.9261 0.01516 0.00973 -0.0009 1.0000 0.0057
-8.750 -0.9060 0.01452 0.00904 0.0003 1.0000 0.0062
-8.500 -0.8835 0.01410 0.00860 0.0011 0.9994 0.0066
-8.000 -0.8208 0.01323 0.00766 -0.0011 0.9871 0.0076
-7.750 -0.7898 0.01281 0.00719 -0.0020 0.9786 0.0081
-7.500 -0.7588 0.01244 0.00677 -0.0030 0.9683 0.0085
-7.250 -0.7296 0.01197 0.00621 -0.0035 0.9534 0.0091
-6.750 -0.6786 0.01131 0.00543 -0.0027 0.9175 0.0107
-6.500 -0.6535 0.01107 0.00513 -0.0022 0.9044 0.0115
-6.250 -0.6282 0.01083 0.00482 -0.0017 0.8931 0.0121
-6.000 -0.6024 0.01060 0.00453 -0.0013 0.8832 0.0125
-5.750 -0.5772 0.01029 0.00414 -0.0008 0.8743 0.0138
-5.500 -0.5516 0.01003 0.00386 -0.0004 0.8660 0.0155
-5.250 -0.5256 0.00981 0.00361 -0.0001 0.8586 0.0172
-5.000 -0.4993 0.00962 0.00338 0.0002 0.8509 0.0187
-4.750 -0.4733 0.00938 0.00313 0.0005 0.8439 0.0228
-4.500 -0.4468 0.00920 0.00292 0.0007 0.8367 0.0261
-4.250 -0.4205 0.00900 0.00272 0.0010 0.8290 0.0322
-4.000 -0.3941 0.00884 0.00253 0.0012 0.8205 0.0378
-3.750 -0.3676 0.00864 0.00235 0.0014 0.8123 0.0472
-3.500 -0.3413 0.00845 0.00218 0.0017 0.8048 0.0597
-3.250 -0.3149 0.00824 0.00202 0.0019 0.7969 0.0766
-3.000 -0.2889 0.00801 0.00187 0.0022 0.7890 0.1037
-2.750 -0.2628 0.00777 0.00174 0.0025 0.7805 0.1350
-2.500 -0.2364 0.00759 0.00161 0.0027 0.7719 0.1603
-2.250 -0.2098 0.00744 0.00150 0.0029 0.7618 0.1823
-2.000 -0.1834 0.00727 0.00140 0.0031 0.7501 0.2110
-1.500 -0.1360 0.00656 0.00112 0.0044 0.7095 0.3708
-1.250 -0.1179 0.00589 0.00093 0.0061 0.6755 0.5442
-0.750 -0.0698 0.00560 0.00083 0.0076 0.6268 0.6539
-0.250 -0.0190 0.00552 0.00079 0.0086 0.5840 0.7154
0.000 0.0064 0.00549 0.00079 0.0091 0.5647 0.7446
0.250 0.0317 0.00547 0.00080 0.0097 0.5452 0.7755
0.500 0.0572 0.00546 0.00083 0.0102 0.5270 0.8064
0.750 0.0828 0.00548 0.00088 0.0108 0.5091 0.8347
1.000 0.1086 0.00553 0.00094 0.0113 0.4892 0.8580
1.250 0.1352 0.00560 0.00099 0.0116 0.4704 0.8731
1.500 0.1623 0.00570 0.00103 0.0117 0.4481 0.8807
1.750 0.1893 0.00583 0.00108 0.0118 0.4229 0.8870
2.000 0.2161 0.00598 0.00114 0.0120 0.3947 0.8933
2.250 0.2423 0.00621 0.00123 0.0122 0.3517 0.8995
2.500 0.2677 0.00653 0.00135 0.0125 0.2992 0.9058
2.750 0.2943 0.00675 0.00147 0.0127 0.2680 0.9111
3.000 0.3211 0.00693 0.00158 0.0128 0.2476 0.9168
3.250 0.3481 0.00708 0.00169 0.0128 0.2319 0.9223
3.500 0.3756 0.00723 0.00181 0.0128 0.2190 0.9275
3.750 0.4027 0.00736 0.00193 0.0129 0.2081 0.9331
4.000 0.4303 0.00751 0.00205 0.0129 0.1976 0.9378
4.250 0.4581 0.00767 0.00220 0.0128 0.1890 0.9427
4.500 0.4851 0.00781 0.00233 0.0128 0.1796 0.9481
4.750 0.5133 0.00799 0.00248 0.0126 0.1693 0.9522
5.000 0.5412 0.00821 0.00265 0.0124 0.1533 0.9565
5.250 0.5679 0.00842 0.00282 0.0125 0.1393 0.9617
5.500 0.5969 0.00863 0.00300 0.0121 0.1280 0.9651
5.750 0.6259 0.00890 0.00320 0.0116 0.1104 0.9686
6.000 0.6502 0.00945 0.00354 0.0119 0.0694 0.9739
6.250 0.6783 0.01001 0.00397 0.0113 0.0404 0.9767
6.500 0.7075 0.01043 0.00433 0.0107 0.0271 0.9794
6.750 0.7359 0.01079 0.00466 0.0102 0.0195 0.9827
7.000 0.7642 0.01115 0.00500 0.0098 0.0150 0.9856
7.250 0.7958 0.01151 0.00536 0.0086 0.0126 0.9870
7.500 0.8268 0.01190 0.00578 0.0076 0.0106 0.9886
7.750 0.8572 0.01223 0.00614 0.0066 0.0096 0.9904
8.000 0.8862 0.01262 0.00654 0.0060 0.0085 0.9925
8.250 0.9139 0.01309 0.00704 0.0055 0.0075 0.9945
8.500 0.9437 0.01352 0.00752 0.0047 0.0070 0.9957
8.750 0.9731 0.01394 0.00798 0.0039 0.0066 0.9970
9.000 1.0018 0.01439 0.00850 0.0031 0.0061 0.9984
9.250 1.0300 0.01488 0.00902 0.0025 0.0057 0.9997
9.500 1.0502 0.01533 0.00951 0.0036 0.0053 1.0000
9.750 1.0662 0.01587 0.01009 0.0055 0.0049 1.0000
10.000 1.0819 0.01646 0.01074 0.0074 0.0046 1.0000
10.250 1.0995 0.01690 0.01124 0.0090 0.0045 1.0000
10.500 1.1167 0.01740 0.01179 0.0106 0.0043 1.0000
10.750 1.1333 0.01796 0.01243 0.0123 0.0041 1.0000
11.000 1.1500 0.01856 0.01310 0.0138 0.0040 1.0000
11.250 1.1667 0.01919 0.01380 0.0153 0.0038 1.0000
11.500 1.1833 0.01985 0.01452 0.0167 0.0036 1.0000
11.750 1.1994 0.02055 0.01528 0.0181 0.0035 1.0000
12.000 1.2149 0.02129 0.01610 0.0195 0.0034 1.0000
12.250 1.2287 0.02209 0.01697 0.0211 0.0033 1.0000
12.500 1.2391 0.02298 0.01793 0.0231 0.0031 1.0000
12.750 1.2472 0.02403 0.01908 0.0252 0.0030 1.0000
13.000 1.2527 0.02534 0.02050 0.0273 0.0029 1.0000
13.250 1.2546 0.02701 0.02232 0.0293 0.0028 1.0000
13.500 1.2549 0.02897 0.02441 0.0308 0.0028 1.0000
13.750 1.2597 0.03067 0.02622 0.0318 0.0027 1.0000
14.000 1.2628 0.03264 0.02831 0.0324 0.0027 1.0000
14.250 1.2649 0.03486 0.03065 0.0328 0.0027 1.0000
14.500 1.2653 0.03740 0.03332 0.0327 0.0027 1.0000
14.750 1.2637 0.04037 0.03641 0.0322 0.0026 1.0000
15.000 1.2596 0.04387 0.04005 0.0312 0.0026 1.0000
15.250 1.2532 0.04792 0.04424 0.0297 0.0026 1.0000
15.500 1.2436 0.05268 0.04914 0.0276 0.0026 1.0000
15.750 1.2312 0.05812 0.05472 0.0249 0.0026 1.0000
16.000 1.2155 0.06433 0.06108 0.0217 0.0026 1.0000
16.250 1.1958 0.07152 0.06842 0.0179 0.0026 1.0000
16.500 1.1734 0.07951 0.07656 0.0136 0.0026 1.0000
16.750 1.1480 0.08832 0.08551 0.0091 0.0026 1.0000
17.000 1.1209 0.09747 0.09479 0.0046 0.0026 1.0000
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