HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Reynolds number: 500,000 Max Cl/Cd: 107.8 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hq300gd2-il-500000-n5.txt Download as CSV file: xf-hq300gd2-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HORSTMANN AND QUAST HQ-300 GD(MOD 2) 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
------ -------- --------- --------- -------- -------- --------
-12.750 -0.6488 0.04782 0.04443 -0.0873 0.8284 0.0098
-12.500 -0.6878 0.04032 0.03647 -0.0896 0.8176 0.0099
-12.250 -0.7046 0.03590 0.03166 -0.0896 0.8078 0.0101
-12.000 -0.7104 0.03266 0.02806 -0.0890 0.7982 0.0103
-11.750 -0.7095 0.03021 0.02529 -0.0881 0.7898 0.0105
-11.500 -0.7015 0.02834 0.02312 -0.0874 0.7814 0.0108
-11.250 -0.6870 0.02691 0.02151 -0.0874 0.7743 0.0110
-11.000 -0.6676 0.02606 0.02056 -0.0876 0.7672 0.0112
-10.500 -0.6248 0.02470 0.01901 -0.0877 0.7548 0.0117
-10.250 -0.6029 0.02392 0.01811 -0.0878 0.7484 0.0120
-10.000 -0.5809 0.02301 0.01704 -0.0878 0.7427 0.0123
-9.750 -0.5584 0.02203 0.01588 -0.0878 0.7368 0.0127
-9.500 -0.5353 0.02108 0.01474 -0.0878 0.7314 0.0132
-9.250 -0.5114 0.02021 0.01369 -0.0878 0.7267 0.0136
-9.000 -0.4868 0.01943 0.01276 -0.0878 0.7216 0.0139
-8.750 -0.4621 0.01872 0.01199 -0.0880 0.7165 0.0143
-8.500 -0.4362 0.01825 0.01144 -0.0883 0.7119 0.0147
-8.250 -0.4096 0.01780 0.01095 -0.0886 0.7070 0.0152
-8.000 -0.3829 0.01737 0.01043 -0.0889 0.7023 0.0158
-7.750 -0.3562 0.01691 0.00987 -0.0891 0.6982 0.0166
-7.500 -0.3291 0.01646 0.00931 -0.0894 0.6943 0.0172
-7.250 -0.3024 0.01587 0.00866 -0.0896 0.6900 0.0177
-7.000 -0.2754 0.01536 0.00811 -0.0900 0.6857 0.0184
-6.750 -0.2479 0.01498 0.00768 -0.0904 0.6817 0.0190
-6.500 -0.2198 0.01462 0.00727 -0.0909 0.6779 0.0197
-6.250 -0.1914 0.01428 0.00689 -0.0914 0.6741 0.0207
-6.000 -0.1628 0.01397 0.00652 -0.0919 0.6704 0.0215
-5.750 -0.1344 0.01354 0.00603 -0.0924 0.6669 0.0224
-5.500 -0.1055 0.01318 0.00564 -0.0931 0.6635 0.0233
-5.250 -0.0761 0.01289 0.00534 -0.0938 0.6598 0.0243
-5.000 -0.0466 0.01264 0.00505 -0.0944 0.6561 0.0257
-4.750 -0.0169 0.01242 0.00477 -0.0951 0.6528 0.0268
-4.500 0.0129 0.01213 0.00445 -0.0959 0.6497 0.0282
-4.250 0.0431 0.01190 0.00420 -0.0967 0.6466 0.0300
-4.000 0.0734 0.01170 0.00400 -0.0975 0.6431 0.0322
-3.750 0.1038 0.01151 0.00379 -0.0983 0.6396 0.0355
-3.500 0.1342 0.01134 0.00361 -0.0991 0.6365 0.0403
-3.250 0.1647 0.01118 0.00345 -0.0999 0.6337 0.0484
-3.000 0.1955 0.01101 0.00331 -0.1009 0.6308 0.0616
-2.750 0.2270 0.01075 0.00316 -0.1020 0.6275 0.0928
-2.500 0.2627 0.00991 0.00292 -0.1049 0.6242 0.2627
-2.250 0.3012 0.00914 0.00273 -0.1084 0.6212 0.4359
-2.000 0.3414 0.00846 0.00267 -0.1120 0.6184 0.6176
-1.750 0.3719 0.00846 0.00289 -0.1125 0.6156 0.6956
-1.500 0.4011 0.00857 0.00304 -0.1127 0.6124 0.7213
-1.250 0.4305 0.00869 0.00314 -0.1130 0.6091 0.7358
-1.000 0.4611 0.00877 0.00317 -0.1137 0.6060 0.7449
-0.750 0.4901 0.00887 0.00322 -0.1140 0.6031 0.7488
-0.500 0.5200 0.00895 0.00327 -0.1145 0.6002 0.7529
-0.250 0.5508 0.00900 0.00329 -0.1153 0.5969 0.7576
0.000 0.5807 0.00907 0.00333 -0.1158 0.5935 0.7614
0.250 0.6091 0.00918 0.00343 -0.1160 0.5903 0.7655
0.500 0.6381 0.00931 0.00352 -0.1163 0.5870 0.7707
0.750 0.6690 0.00938 0.00356 -0.1171 0.5833 0.7754
1.000 0.6982 0.00944 0.00363 -0.1175 0.5789 0.7775
1.250 0.7269 0.00952 0.00369 -0.1178 0.5744 0.7793
1.500 0.7557 0.00962 0.00374 -0.1182 0.5702 0.7811
1.750 0.7852 0.00967 0.00382 -0.1187 0.5658 0.7831
2.000 0.8146 0.00974 0.00389 -0.1192 0.5611 0.7852
2.250 0.8442 0.00983 0.00394 -0.1198 0.5567 0.7873
2.500 0.8741 0.00990 0.00401 -0.1205 0.5526 0.7895
2.750 0.9044 0.00997 0.00408 -0.1213 0.5478 0.7916
3.000 0.9332 0.01005 0.00416 -0.1217 0.5430 0.7930
3.250 0.9614 0.01016 0.00427 -0.1220 0.5385 0.7943
3.500 0.9900 0.01024 0.00439 -0.1223 0.5334 0.7958
3.750 1.0183 0.01034 0.00450 -0.1226 0.5278 0.7973
4.000 1.0466 0.01046 0.00461 -0.1230 0.5226 0.7988
4.250 1.0752 0.01055 0.00475 -0.1234 0.5160 0.8004
4.500 1.1031 0.01069 0.00487 -0.1237 0.5094 0.8023
4.750 1.1317 0.01081 0.00501 -0.1241 0.5019 0.8041
5.000 1.1595 0.01097 0.00516 -0.1245 0.4937 0.8059
5.250 1.1879 0.01111 0.00531 -0.1249 0.4844 0.8075
5.500 1.2148 0.01129 0.00549 -0.1251 0.4743 0.8089
5.750 1.2403 0.01151 0.00570 -0.1249 0.4627 0.8102
6.000 1.2656 0.01174 0.00593 -0.1248 0.4492 0.8115
6.250 1.2902 0.01202 0.00619 -0.1245 0.4345 0.8129
6.500 1.3140 0.01235 0.00649 -0.1242 0.4186 0.8143
6.750 1.3367 0.01275 0.00683 -0.1236 0.4011 0.8158
7.000 1.3589 0.01317 0.00721 -0.1231 0.3836 0.8175
7.250 1.3801 0.01363 0.00762 -0.1223 0.3660 0.8194
7.500 1.4004 0.01414 0.00808 -0.1215 0.3487 0.8213
7.750 1.4199 0.01467 0.00856 -0.1205 0.3325 0.8231
8.000 1.4381 0.01521 0.00907 -0.1194 0.3175 0.8246
8.250 1.4543 0.01577 0.00962 -0.1178 0.3038 0.8258
8.500 1.4664 0.01638 0.01021 -0.1155 0.2907 0.8273
8.750 1.4764 0.01706 0.01089 -0.1130 0.2783 0.8291
9.000 1.4870 0.01793 0.01173 -0.1108 0.2628 0.8310
9.250 1.4943 0.01906 0.01279 -0.1085 0.2422 0.8330
9.500 1.4982 0.02051 0.01413 -0.1061 0.2202 0.8350
9.750 1.5037 0.02199 0.01553 -0.1041 0.1993 0.8369
10.000 1.5108 0.02345 0.01695 -0.1025 0.1838 0.8387
10.250 1.5182 0.02495 0.01842 -0.1010 0.1709 0.8403
10.500 1.5245 0.02652 0.01999 -0.0994 0.1589 0.8418
10.750 1.5296 0.02825 0.02170 -0.0979 0.1468 0.8434
11.000 1.5337 0.03011 0.02355 -0.0964 0.1349 0.8450
11.250 1.5369 0.03209 0.02552 -0.0949 0.1228 0.8466
11.500 1.5404 0.03409 0.02751 -0.0936 0.1116 0.8482
11.750 1.5430 0.03621 0.02962 -0.0923 0.1007 0.8498
12.000 1.5449 0.03843 0.03184 -0.0910 0.0904 0.8513
12.250 1.5454 0.04080 0.03419 -0.0897 0.0803 0.8529
12.500 1.5452 0.04330 0.03668 -0.0885 0.0703 0.8545
12.750 1.5445 0.04590 0.03926 -0.0874 0.0608 0.8559
13.000 1.5430 0.04859 0.04195 -0.0863 0.0520 0.8573
13.250 1.5417 0.05135 0.04473 -0.0853 0.0443 0.8586
13.500 1.5409 0.05415 0.04754 -0.0844 0.0379 0.8598
13.750 1.5405 0.05696 0.05038 -0.0837 0.0326 0.8612
14.000 1.5407 0.05975 0.05321 -0.0831 0.0286 0.8625
14.250 1.5400 0.06271 0.05621 -0.0826 0.0251 0.8639
14.500 1.5410 0.06555 0.05911 -0.0822 0.0225 0.8653
14.750 1.5404 0.06859 0.06221 -0.0818 0.0204 0.8666
15.000 1.5415 0.07149 0.06517 -0.0816 0.0187 0.8680
15.250 1.5407 0.07466 0.06841 -0.0814 0.0173 0.8694
15.500 1.5400 0.07785 0.07167 -0.0813 0.0161 0.8707
15.750 1.5401 0.08094 0.07487 -0.0812 0.0151 0.8720
16.000 1.5386 0.08429 0.07830 -0.0812 0.0143 0.8733
16.250 1.5360 0.08778 0.08188 -0.0813 0.0135 0.8746
16.500 1.5335 0.09135 0.08554 -0.0815 0.0130 0.8759
16.750 1.5319 0.09487 0.08916 -0.0819 0.0125 0.8772
17.000 1.5297 0.09849 0.09288 -0.0823 0.0120 0.8785
17.250 1.5268 0.10225 0.09674 -0.0829 0.0115 0.8799
17.500 1.5226 0.10624 0.10082 -0.0836 0.0111 0.8812
17.750 1.5174 0.11043 0.10509 -0.0844 0.0107 0.8825
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