GIII BL45 AIRFOIL (giiib-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GIII BL45 AIRFOIL (giiib-il) Reynolds number: 500,000 Max Cl/Cd: 61.85 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-giiib-il-500000-n5.txt Download as CSV file: xf-giiib-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.250 -0.7945 0.10466 0.10250 0.0056 1.0000 0.0059
-13.000 -0.9405 0.06122 0.05876 -0.0223 1.0000 0.0052
-12.750 -0.9699 0.05237 0.04967 -0.0285 1.0000 0.0052
-12.500 -0.9935 0.04656 0.04361 -0.0302 1.0000 0.0052
-12.250 -1.0123 0.04222 0.03901 -0.0295 1.0000 0.0052
-12.000 -1.0261 0.03878 0.03530 -0.0274 1.0000 0.0053
-11.750 -1.0347 0.03595 0.03220 -0.0245 1.0000 0.0053
-11.500 -1.0381 0.03353 0.02951 -0.0215 1.0000 0.0054
-11.250 -1.0343 0.03135 0.02706 -0.0191 1.0000 0.0055
-11.000 -1.0259 0.02946 0.02492 -0.0172 1.0000 0.0057
-10.750 -1.0163 0.02757 0.02278 -0.0152 1.0000 0.0058
-10.500 -1.0048 0.02588 0.02091 -0.0134 1.0000 0.0060
-10.250 -0.9874 0.02493 0.01985 -0.0123 1.0000 0.0063
-10.000 -0.9682 0.02417 0.01901 -0.0114 1.0000 0.0066
-9.750 -0.9487 0.02339 0.01813 -0.0104 1.0000 0.0069
-9.500 -0.9294 0.02252 0.01713 -0.0093 1.0000 0.0073
-9.250 -0.9102 0.02154 0.01598 -0.0082 1.0000 0.0076
-9.000 -0.8910 0.02054 0.01482 -0.0070 1.0000 0.0080
-8.750 -0.8713 0.01963 0.01376 -0.0058 1.0000 0.0083
-8.500 -0.8508 0.01887 0.01288 -0.0046 1.0000 0.0086
-8.250 -0.8336 0.01771 0.01161 -0.0030 1.0000 0.0091
-8.000 -0.8140 0.01704 0.01088 -0.0017 1.0000 0.0096
-7.750 -0.7940 0.01650 0.01029 -0.0004 1.0000 0.0101
-7.500 -0.7743 0.01605 0.00979 0.0010 1.0000 0.0108
-7.250 -0.7454 0.01551 0.00917 0.0004 0.9961 0.0117
-7.000 -0.7136 0.01500 0.00856 -0.0008 0.9903 0.0124
-6.750 -0.6838 0.01414 0.00762 -0.0016 0.9835 0.0135
-6.500 -0.6528 0.01357 0.00702 -0.0026 0.9757 0.0146
-6.250 -0.6217 0.01314 0.00655 -0.0035 0.9661 0.0160
-6.000 -0.5909 0.01275 0.00610 -0.0043 0.9554 0.0174
-5.750 -0.5617 0.01234 0.00561 -0.0048 0.9443 0.0186
-5.500 -0.5348 0.01185 0.00508 -0.0047 0.9332 0.0212
-5.250 -0.5085 0.01154 0.00473 -0.0044 0.9220 0.0240
-5.000 -0.4826 0.01127 0.00440 -0.0040 0.9113 0.0270
-4.750 -0.4575 0.01094 0.00404 -0.0035 0.9012 0.0326
-4.250 -0.4066 0.01044 0.00349 -0.0025 0.8825 0.0472
-4.000 -0.3812 0.01018 0.00325 -0.0021 0.8739 0.0605
-3.750 -0.3563 0.00988 0.00302 -0.0016 0.8653 0.0832
-3.500 -0.3312 0.00959 0.00281 -0.0011 0.8567 0.1127
-3.250 -0.3061 0.00934 0.00263 -0.0007 0.8479 0.1431
-3.000 -0.2807 0.00909 0.00246 -0.0002 0.8386 0.1726
-2.750 -0.2552 0.00885 0.00230 0.0002 0.8299 0.2022
-2.500 -0.2302 0.00857 0.00213 0.0006 0.8214 0.2460
-2.250 -0.2076 0.00802 0.00193 0.0014 0.8128 0.3432
-2.000 -0.1908 0.00709 0.00169 0.0033 0.8040 0.5293
-1.750 -0.1694 0.00667 0.00160 0.0046 0.7947 0.6259
-1.500 -0.1460 0.00643 0.00154 0.0056 0.7857 0.6837
-1.250 -0.1210 0.00629 0.00149 0.0064 0.7760 0.7215
-1.000 -0.0957 0.00618 0.00146 0.0070 0.7641 0.7529
-0.750 -0.0705 0.00613 0.00142 0.0078 0.7430 0.7811
-0.500 -0.0456 0.00614 0.00138 0.0086 0.7139 0.8075
-0.250 -0.0202 0.00618 0.00138 0.0094 0.6884 0.8311
0.000 0.0058 0.00623 0.00140 0.0100 0.6674 0.8522
0.250 0.0317 0.00632 0.00144 0.0106 0.6460 0.8719
0.500 0.0578 0.00642 0.00149 0.0112 0.6232 0.8880
0.750 0.0846 0.00654 0.00152 0.0115 0.6008 0.8975
1.000 0.1115 0.00663 0.00154 0.0117 0.5813 0.9046
1.250 0.1394 0.00673 0.00158 0.0117 0.5637 0.9101
1.500 0.1670 0.00685 0.00163 0.0118 0.5443 0.9159
1.750 0.1938 0.00697 0.00168 0.0120 0.5228 0.9218
2.000 0.2225 0.00711 0.00175 0.0118 0.5020 0.9263
2.250 0.2498 0.00724 0.00182 0.0118 0.4800 0.9321
2.500 0.2774 0.00740 0.00190 0.0118 0.4536 0.9369
2.750 0.3062 0.00762 0.00201 0.0115 0.4206 0.9409
3.000 0.3326 0.00789 0.00212 0.0116 0.3779 0.9463
3.250 0.3588 0.00828 0.00229 0.0117 0.3187 0.9509
3.500 0.3879 0.00863 0.00248 0.0112 0.2801 0.9543
3.750 0.4163 0.00890 0.00266 0.0108 0.2565 0.9585
4.000 0.4433 0.00912 0.00283 0.0108 0.2396 0.9633
4.250 0.4749 0.00935 0.00303 0.0098 0.2247 0.9656
4.500 0.5057 0.00958 0.00323 0.0090 0.2122 0.9685
4.750 0.5349 0.00980 0.00343 0.0085 0.2017 0.9722
5.000 0.5643 0.01004 0.00364 0.0079 0.1886 0.9755
5.250 0.5969 0.01031 0.00387 0.0066 0.1725 0.9772
5.500 0.6288 0.01058 0.00409 0.0054 0.1538 0.9794
5.750 0.6594 0.01085 0.00432 0.0045 0.1386 0.9822
6.000 0.6884 0.01113 0.00457 0.0039 0.1227 0.9854
6.250 0.7192 0.01168 0.00493 0.0027 0.0822 0.9872
6.500 0.7474 0.01251 0.00552 0.0018 0.0405 0.9896
6.750 0.7769 0.01303 0.00600 0.0010 0.0276 0.9922
7.000 0.8062 0.01351 0.00648 0.0002 0.0208 0.9947
7.250 0.8366 0.01406 0.00705 -0.0008 0.0159 0.9964
7.500 0.8670 0.01449 0.00755 -0.0018 0.0142 0.9983
7.750 0.8961 0.01501 0.00812 -0.0026 0.0126 1.0000
8.000 0.9127 0.01558 0.00872 -0.0007 0.0113 1.0000
8.250 0.9290 0.01614 0.00936 0.0012 0.0105 1.0000
8.500 0.9464 0.01659 0.00988 0.0029 0.0098 1.0000
8.750 0.9634 0.01709 0.01043 0.0047 0.0090 1.0000
9.000 0.9798 0.01764 0.01107 0.0065 0.0085 1.0000
9.250 0.9955 0.01828 0.01176 0.0084 0.0080 1.0000
9.500 1.0086 0.01914 0.01270 0.0106 0.0075 1.0000
9.750 1.0210 0.02005 0.01370 0.0129 0.0071 1.0000
10.000 1.0358 0.02079 0.01454 0.0147 0.0069 1.0000
10.250 1.0499 0.02162 0.01547 0.0166 0.0067 1.0000
10.500 1.0633 0.02253 0.01649 0.0185 0.0064 1.0000
10.750 1.0763 0.02347 0.01754 0.0203 0.0061 1.0000
11.000 1.0890 0.02441 0.01857 0.0220 0.0058 1.0000
11.250 1.0999 0.02531 0.01959 0.0240 0.0056 1.0000
11.500 1.1099 0.02624 0.02059 0.0259 0.0053 1.0000
11.750 1.1185 0.02732 0.02176 0.0277 0.0051 1.0000
12.000 1.1247 0.02866 0.02320 0.0295 0.0049 1.0000
12.250 1.1257 0.03056 0.02522 0.0312 0.0048 1.0000
12.500 1.1244 0.03282 0.02763 0.0326 0.0047 1.0000
12.750 1.1271 0.03487 0.02983 0.0334 0.0046 1.0000
13.000 1.1282 0.03720 0.03232 0.0339 0.0045 1.0000
13.250 1.1278 0.03986 0.03514 0.0340 0.0045 1.0000
13.500 1.1252 0.04296 0.03840 0.0336 0.0044 1.0000
13.750 1.1207 0.04651 0.04212 0.0327 0.0043 1.0000
14.000 1.1142 0.05057 0.04635 0.0312 0.0043 1.0000
14.250 1.1058 0.05517 0.05112 0.0292 0.0043 1.0000
14.500 1.0951 0.06036 0.05647 0.0267 0.0042 1.0000
14.750 1.0824 0.06615 0.06243 0.0236 0.0042 1.0000
15.000 1.0675 0.07256 0.06900 0.0201 0.0042 1.0000
15.250 1.0510 0.07960 0.07619 0.0162 0.0042 1.0000
15.500 1.0331 0.08720 0.08394 0.0120 0.0042 1.0000
15.750 1.0142 0.09523 0.09211 0.0077 0.0042 1.0000
16.000 0.9944 0.10358 0.10059 0.0033 0.0042 1.0000
16.250 0.9738 0.11220 0.10933 -0.0011 0.0043 1.0000
16.500 0.9530 0.12113 0.11837 -0.0057 0.0043 1.0000
16.750 0.9315 0.13045 0.12780 -0.0104 0.0043 1.0000
17.000 0.9088 0.14054 0.13799 -0.0155 0.0044 1.0000
17.250 0.8819 0.15243 0.14999 -0.0214 0.0044 1.0000
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