GIII BL75 AIRFOIL (giiic-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GIII BL75 AIRFOIL (giiic-il) Reynolds number: 1,000,000 Max Cl/Cd: 71.02 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-giiic-il-1000000-n5.txt Download as CSV file: xf-giiic-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GIII BL75 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
------ -------- --------- --------- -------- -------- --------
-14.250 -1.0907 0.05837 0.05648 -0.0196 1.0000 0.0029
-14.000 -1.1301 0.04820 0.04603 -0.0264 1.0000 0.0029
-13.750 -1.1524 0.04288 0.04049 -0.0274 1.0000 0.0029
-13.500 -1.1670 0.03917 0.03658 -0.0264 1.0000 0.0029
-13.250 -1.1761 0.03633 0.03355 -0.0244 1.0000 0.0030
-13.000 -1.1807 0.03401 0.03104 -0.0219 1.0000 0.0030
-12.750 -1.1802 0.03201 0.02886 -0.0194 1.0000 0.0031
-12.500 -1.1740 0.03011 0.02677 -0.0175 1.0000 0.0031
-12.250 -1.1642 0.02841 0.02487 -0.0159 1.0000 0.0032
-12.000 -1.1521 0.02685 0.02313 -0.0144 1.0000 0.0033
-11.750 -1.1378 0.02546 0.02157 -0.0131 1.0000 0.0033
-11.500 -1.1219 0.02417 0.02012 -0.0119 1.0000 0.0034
-11.250 -1.1045 0.02301 0.01881 -0.0108 1.0000 0.0035
-11.000 -1.0858 0.02197 0.01762 -0.0099 1.0000 0.0035
-10.750 -1.0663 0.02100 0.01652 -0.0090 1.0000 0.0036
-10.500 -1.0461 0.02008 0.01547 -0.0081 1.0000 0.0037
-10.250 -1.0283 0.01873 0.01394 -0.0069 1.0000 0.0039
-10.000 -1.0072 0.01785 0.01296 -0.0061 1.0000 0.0041
-9.750 -0.9848 0.01717 0.01219 -0.0055 1.0000 0.0043
-9.500 -0.9618 0.01658 0.01153 -0.0049 1.0000 0.0045
-9.250 -0.9385 0.01603 0.01092 -0.0043 1.0000 0.0048
-9.000 -0.9151 0.01548 0.01031 -0.0038 1.0000 0.0050
-8.750 -0.8866 0.01491 0.00967 -0.0043 0.9837 0.0053
-8.500 -0.8539 0.01438 0.00904 -0.0057 0.9556 0.0056
-8.250 -0.8275 0.01401 0.00856 -0.0056 0.9256 0.0059
-8.000 -0.8047 0.01353 0.00792 -0.0048 0.9046 0.0063
-7.750 -0.7808 0.01310 0.00741 -0.0041 0.8906 0.0068
-7.250 -0.7308 0.01245 0.00661 -0.0033 0.8684 0.0078
-7.000 -0.7055 0.01213 0.00621 -0.0029 0.8585 0.0083
-6.750 -0.6800 0.01184 0.00584 -0.0025 0.8499 0.0088
-6.500 -0.6539 0.01156 0.00550 -0.0023 0.8431 0.0091
-6.250 -0.6288 0.01112 0.00497 -0.0018 0.8372 0.0101
-6.000 -0.6028 0.01082 0.00465 -0.0016 0.8320 0.0111
-5.750 -0.5765 0.01056 0.00436 -0.0014 0.8266 0.0120
-5.500 -0.5502 0.01032 0.00406 -0.0011 0.8217 0.0128
-5.250 -0.5235 0.01008 0.00379 -0.0010 0.8167 0.0134
-5.000 -0.4971 0.00982 0.00348 -0.0008 0.8118 0.0147
-4.750 -0.4706 0.00956 0.00320 -0.0005 0.8071 0.0170
-4.500 -0.4437 0.00935 0.00297 -0.0004 0.8021 0.0192
-4.250 -0.4168 0.00915 0.00275 -0.0003 0.7971 0.0224
-4.000 -0.3901 0.00894 0.00255 -0.0001 0.7925 0.0282
-3.750 -0.3631 0.00873 0.00235 0.0000 0.7871 0.0356
-3.500 -0.3362 0.00854 0.00218 0.0001 0.7816 0.0450
-3.250 -0.3094 0.00834 0.00201 0.0003 0.7764 0.0588
-3.000 -0.2825 0.00813 0.00186 0.0004 0.7703 0.0770
-2.750 -0.2558 0.00794 0.00172 0.0005 0.7643 0.0972
-2.500 -0.2290 0.00772 0.00159 0.0006 0.7576 0.1241
-2.000 -0.1756 0.00730 0.00137 0.0009 0.7435 0.1901
-1.750 -0.1491 0.00710 0.00125 0.0011 0.7360 0.2268
-1.500 -0.1236 0.00675 0.00114 0.0014 0.7266 0.3002
-1.250 -0.0993 0.00632 0.00100 0.0019 0.7141 0.3981
-1.000 -0.0800 0.00551 0.00084 0.0033 0.6965 0.5995
-0.750 -0.0547 0.00537 0.00077 0.0038 0.6758 0.6481
-0.500 -0.0291 0.00527 0.00074 0.0042 0.6566 0.6883
-0.250 -0.0028 0.00523 0.00072 0.0046 0.6387 0.7162
0.000 0.0236 0.00520 0.00071 0.0049 0.6215 0.7423
0.250 0.0499 0.00518 0.00072 0.0052 0.6029 0.7696
0.500 0.0761 0.00519 0.00074 0.0056 0.5835 0.7956
1.000 0.1280 0.00522 0.00083 0.0065 0.5496 0.8513
1.250 0.1546 0.00527 0.00088 0.0068 0.5330 0.8680
1.500 0.1821 0.00535 0.00092 0.0069 0.5157 0.8752
1.750 0.2097 0.00543 0.00096 0.0069 0.4987 0.8813
2.000 0.2369 0.00554 0.00102 0.0070 0.4756 0.8876
2.250 0.2640 0.00569 0.00107 0.0071 0.4464 0.8937
2.500 0.2907 0.00587 0.00116 0.0072 0.4112 0.8999
2.750 0.3166 0.00617 0.00128 0.0074 0.3587 0.9067
3.000 0.3426 0.00646 0.00142 0.0076 0.3144 0.9127
3.250 0.3693 0.00666 0.00154 0.0078 0.2895 0.9194
3.500 0.3961 0.00686 0.00168 0.0078 0.2660 0.9254
3.750 0.4231 0.00702 0.00181 0.0079 0.2477 0.9321
4.000 0.4498 0.00727 0.00196 0.0080 0.2199 0.9382
4.250 0.4766 0.00752 0.00213 0.0080 0.1949 0.9446
4.500 0.5033 0.00777 0.00230 0.0081 0.1707 0.9509
4.750 0.5311 0.00804 0.00248 0.0079 0.1464 0.9563
5.000 0.5580 0.00830 0.00267 0.0079 0.1276 0.9625
5.250 0.5870 0.00860 0.00290 0.0073 0.1050 0.9667
5.500 0.6143 0.00907 0.00320 0.0071 0.0703 0.9717
5.750 0.6417 0.00954 0.00355 0.0067 0.0429 0.9763
6.000 0.6716 0.00993 0.00387 0.0059 0.0297 0.9795
6.250 0.7004 0.01027 0.00417 0.0054 0.0216 0.9836
6.500 0.7303 0.01059 0.00450 0.0047 0.0165 0.9865
6.750 0.7617 0.01096 0.00485 0.0035 0.0134 0.9886
7.000 0.7926 0.01129 0.00521 0.0025 0.0116 0.9909
7.250 0.8225 0.01162 0.00556 0.0017 0.0104 0.9934
7.500 0.8524 0.01202 0.00596 0.0009 0.0091 0.9953
7.750 0.8825 0.01249 0.00648 0.0000 0.0079 0.9969
8.000 0.9126 0.01285 0.00689 -0.0010 0.0075 0.9986
8.250 0.9414 0.01326 0.00734 -0.0016 0.0069 1.0000
8.500 0.9611 0.01364 0.00775 -0.0003 0.0064 1.0000
8.750 0.9810 0.01405 0.00819 0.0010 0.0059 1.0000
9.000 1.0001 0.01456 0.00874 0.0023 0.0054 1.0000
9.250 1.0194 0.01508 0.00931 0.0036 0.0050 1.0000
9.500 1.0399 0.01551 0.00980 0.0046 0.0048 1.0000
9.750 1.0603 0.01600 0.01035 0.0057 0.0046 1.0000
10.000 1.0806 0.01654 0.01095 0.0066 0.0043 1.0000
10.250 1.1009 0.01710 0.01157 0.0076 0.0041 1.0000
10.500 1.1211 0.01768 0.01221 0.0084 0.0039 1.0000
10.750 1.1410 0.01830 0.01289 0.0093 0.0037 1.0000
11.000 1.1601 0.01900 0.01364 0.0102 0.0035 1.0000
11.250 1.1777 0.01982 0.01454 0.0113 0.0033 1.0000
11.500 1.1923 0.02092 0.01578 0.0127 0.0031 1.0000
11.750 1.2057 0.02205 0.01703 0.0142 0.0030 1.0000
12.000 1.2209 0.02295 0.01802 0.0154 0.0030 1.0000
12.250 1.2334 0.02388 0.01905 0.0169 0.0029 1.0000
12.500 1.2435 0.02491 0.02020 0.0187 0.0029 1.0000
12.750 1.2521 0.02609 0.02148 0.0204 0.0028 1.0000
13.000 1.2592 0.02745 0.02296 0.0218 0.0028 1.0000
13.250 1.2655 0.02897 0.02460 0.0230 0.0027 1.0000
13.500 1.2696 0.03077 0.02652 0.0240 0.0027 1.0000
13.750 1.2727 0.03277 0.02866 0.0247 0.0026 1.0000
14.000 1.2745 0.03500 0.03101 0.0252 0.0026 1.0000
14.250 1.2740 0.03759 0.03374 0.0253 0.0025 1.0000
14.500 1.2721 0.04052 0.03682 0.0251 0.0025 1.0000
14.750 1.2681 0.04388 0.04032 0.0244 0.0024 1.0000
15.000 1.2615 0.04781 0.04439 0.0231 0.0024 1.0000
15.250 1.2519 0.05242 0.04916 0.0213 0.0024 1.0000
15.500 1.2403 0.05766 0.05454 0.0188 0.0024 1.0000
15.750 1.2239 0.06396 0.06100 0.0155 0.0024 1.0000
16.000 1.2043 0.07126 0.06845 0.0115 0.0023 1.0000
16.250 1.1800 0.07994 0.07729 0.0067 0.0024 1.0000
16.500 1.1513 0.08984 0.08736 0.0014 0.0024 1.0000
16.750 1.1193 0.10042 0.09807 -0.0041 0.0024 1.0000
17.000 1.0868 0.11114 0.10892 -0.0094 0.0025 1.0000
17.250 1.0538 0.12227 0.12016 -0.0150 0.0025 1.0000
17.500 1.0228 0.13338 0.13139 -0.0205 0.0025 1.0000
17.750 0.9914 0.14524 0.14336 -0.0265 0.0026 1.0000
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