HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Reynolds number: 1,000,000 Max Cl/Cd: 131.6 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hq300gd2-il-1000000-n5.txt Download as CSV file: xf-hq300gd2-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.250 -0.9565 0.05040 0.04756 -0.0814 1.0000 0.0068
-16.000 -0.9681 0.04548 0.04249 -0.0843 1.0000 0.0068
-15.750 -0.9721 0.04165 0.03844 -0.0868 0.9335 0.0069
-15.500 -0.9770 0.03881 0.03534 -0.0871 0.8970 0.0069
-15.250 -0.9770 0.03641 0.03274 -0.0873 0.8754 0.0070
-14.750 -0.9692 0.03241 0.02840 -0.0872 0.8458 0.0072
-14.500 -0.9624 0.03072 0.02657 -0.0869 0.8336 0.0073
-14.250 -0.9538 0.02923 0.02492 -0.0866 0.8223 0.0073
-14.000 -0.9436 0.02787 0.02342 -0.0862 0.8112 0.0075
-13.750 -0.9320 0.02660 0.02202 -0.0857 0.8015 0.0076
-13.500 -0.9190 0.02546 0.02074 -0.0852 0.7927 0.0077
-13.250 -0.9049 0.02439 0.01956 -0.0847 0.7843 0.0078
-13.000 -0.8910 0.02347 0.01850 -0.0840 0.7761 0.0079
-12.750 -0.8744 0.02258 0.01751 -0.0836 0.7681 0.0080
-12.500 -0.8549 0.02175 0.01655 -0.0836 0.7606 0.0081
-12.250 -0.8337 0.02098 0.01566 -0.0838 0.7537 0.0082
-12.000 -0.8129 0.02010 0.01468 -0.0839 0.7471 0.0084
-11.750 -0.7903 0.01939 0.01388 -0.0840 0.7414 0.0086
-11.500 -0.7665 0.01881 0.01324 -0.0842 0.7351 0.0089
-11.000 -0.7171 0.01781 0.01210 -0.0846 0.7234 0.0093
-10.750 -0.6917 0.01734 0.01156 -0.0848 0.7175 0.0096
-10.500 -0.6662 0.01689 0.01103 -0.0850 0.7125 0.0098
-10.250 -0.6400 0.01644 0.01053 -0.0853 0.7079 0.0101
-10.000 -0.6136 0.01602 0.01004 -0.0856 0.7029 0.0104
-9.750 -0.5870 0.01564 0.00958 -0.0859 0.6978 0.0107
-9.500 -0.5604 0.01517 0.00904 -0.0862 0.6934 0.0110
-9.250 -0.5332 0.01476 0.00860 -0.0866 0.6886 0.0114
-9.000 -0.5057 0.01444 0.00824 -0.0870 0.6841 0.0118
-8.750 -0.4779 0.01414 0.00789 -0.0874 0.6801 0.0122
-8.500 -0.4497 0.01383 0.00754 -0.0879 0.6765 0.0126
-8.250 -0.4215 0.01351 0.00718 -0.0884 0.6723 0.0130
-8.000 -0.3932 0.01322 0.00683 -0.0889 0.6680 0.0134
-7.750 -0.3647 0.01295 0.00650 -0.0894 0.6641 0.0137
-7.500 -0.3360 0.01259 0.00610 -0.0899 0.6606 0.0142
-7.250 -0.3070 0.01231 0.00581 -0.0905 0.6570 0.0148
-7.000 -0.2779 0.01210 0.00558 -0.0911 0.6533 0.0154
-6.750 -0.2487 0.01189 0.00533 -0.0917 0.6497 0.0161
-6.500 -0.2192 0.01165 0.00505 -0.0924 0.6465 0.0166
-6.250 -0.1895 0.01142 0.00480 -0.0930 0.6429 0.0171
-6.000 -0.1597 0.01123 0.00457 -0.0937 0.6393 0.0175
-5.750 -0.1298 0.01092 0.00423 -0.0945 0.6360 0.0184
-5.500 -0.0999 0.01073 0.00402 -0.0952 0.6329 0.0193
-5.250 -0.0696 0.01055 0.00383 -0.0960 0.6301 0.0201
-5.000 -0.0392 0.01037 0.00362 -0.0968 0.6268 0.0209
-4.750 -0.0088 0.01021 0.00344 -0.0975 0.6233 0.0215
-4.500 0.0216 0.01004 0.00324 -0.0983 0.6200 0.0227
-4.250 0.0522 0.00989 0.00307 -0.0991 0.6171 0.0241
-4.000 0.0830 0.00974 0.00293 -0.1000 0.6146 0.0254
-3.750 0.1137 0.00962 0.00279 -0.1008 0.6116 0.0268
-3.500 0.1446 0.00948 0.00266 -0.1017 0.6084 0.0297
-3.250 0.1754 0.00937 0.00255 -0.1025 0.6052 0.0341
-3.000 0.2062 0.00926 0.00246 -0.1034 0.6024 0.0422
-2.750 0.2374 0.00913 0.00237 -0.1043 0.5999 0.0537
-2.500 0.2688 0.00899 0.00229 -0.1053 0.5971 0.0709
-2.250 0.3009 0.00877 0.00219 -0.1066 0.5940 0.1112
-2.000 0.3387 0.00803 0.00202 -0.1098 0.5909 0.2905
-1.750 0.3759 0.00753 0.00191 -0.1127 0.5878 0.4227
-1.500 0.4163 0.00694 0.00181 -0.1163 0.5849 0.5806
-1.250 0.4515 0.00671 0.00188 -0.1182 0.5822 0.6760
-1.000 0.4825 0.00673 0.00195 -0.1189 0.5791 0.7079
-0.750 0.5128 0.00678 0.00200 -0.1195 0.5759 0.7194
-0.500 0.5432 0.00685 0.00202 -0.1202 0.5726 0.7270
-0.250 0.5733 0.00690 0.00205 -0.1208 0.5693 0.7310
0.000 0.6036 0.00694 0.00209 -0.1214 0.5655 0.7350
0.250 0.6338 0.00700 0.00212 -0.1220 0.5607 0.7392
0.500 0.6639 0.00708 0.00214 -0.1226 0.5560 0.7432
0.750 0.6937 0.00714 0.00221 -0.1232 0.5519 0.7472
1.000 0.7234 0.00721 0.00228 -0.1237 0.5473 0.7528
1.250 0.7533 0.00730 0.00234 -0.1243 0.5426 0.7578
1.500 0.7831 0.00738 0.00239 -0.1248 0.5384 0.7606
1.750 0.8127 0.00743 0.00245 -0.1254 0.5342 0.7626
2.000 0.8423 0.00750 0.00252 -0.1259 0.5294 0.7645
2.250 0.8715 0.00760 0.00260 -0.1264 0.5245 0.7664
2.500 0.9012 0.00767 0.00267 -0.1270 0.5201 0.7682
2.750 0.9307 0.00775 0.00274 -0.1275 0.5146 0.7701
3.000 0.9598 0.00786 0.00282 -0.1280 0.5091 0.7720
3.250 0.9894 0.00794 0.00291 -0.1286 0.5033 0.7737
3.500 1.0185 0.00806 0.00300 -0.1291 0.4962 0.7752
3.750 1.0474 0.00817 0.00310 -0.1295 0.4892 0.7767
4.000 1.0757 0.00829 0.00322 -0.1299 0.4806 0.7782
4.250 1.1041 0.00843 0.00334 -0.1302 0.4713 0.7796
4.500 1.1319 0.00861 0.00349 -0.1305 0.4608 0.7810
4.750 1.1594 0.00881 0.00366 -0.1308 0.4483 0.7826
5.000 1.1865 0.00903 0.00384 -0.1309 0.4337 0.7842
5.250 1.2131 0.00930 0.00405 -0.1310 0.4178 0.7857
5.500 1.2392 0.00960 0.00428 -0.1311 0.4010 0.7872
5.750 1.2648 0.00992 0.00454 -0.1311 0.3834 0.7887
6.000 1.2899 0.01027 0.00482 -0.1309 0.3651 0.7902
6.250 1.3146 0.01065 0.00511 -0.1308 0.3477 0.7916
6.500 1.3388 0.01101 0.00543 -0.1305 0.3315 0.7930
6.750 1.3624 0.01140 0.00576 -0.1301 0.3158 0.7943
7.000 1.3858 0.01178 0.00610 -0.1297 0.3016 0.7956
7.250 1.4087 0.01217 0.00646 -0.1292 0.2879 0.7969
7.500 1.4310 0.01258 0.00683 -0.1287 0.2749 0.7984
7.750 1.4524 0.01302 0.00722 -0.1279 0.2619 0.8000
8.000 1.4720 0.01353 0.00767 -0.1269 0.2459 0.8016
8.250 1.4881 0.01420 0.00824 -0.1254 0.2242 0.8032
8.500 1.4984 0.01508 0.00896 -0.1229 0.1968 0.8048
8.750 1.5025 0.01595 0.00972 -0.1192 0.1757 0.8064
9.000 1.5132 0.01677 0.01048 -0.1170 0.1615 0.8079
9.250 1.5241 0.01764 0.01132 -0.1150 0.1493 0.8096
9.500 1.5338 0.01863 0.01229 -0.1129 0.1367 0.8113
9.750 1.5430 0.01975 0.01337 -0.1110 0.1245 0.8128
10.000 1.5514 0.02099 0.01459 -0.1092 0.1127 0.8144
10.250 1.5601 0.02229 0.01588 -0.1076 0.1023 0.8159
10.500 1.5668 0.02379 0.01735 -0.1059 0.0912 0.8174
10.750 1.5724 0.02545 0.01897 -0.1043 0.0802 0.8190
11.000 1.5764 0.02727 0.02076 -0.1026 0.0691 0.8207
11.250 1.5796 0.02922 0.02268 -0.1010 0.0587 0.8223
11.500 1.5826 0.03123 0.02466 -0.0995 0.0497 0.8237
11.750 1.5847 0.03334 0.02676 -0.0980 0.0416 0.8250
12.000 1.5867 0.03548 0.02891 -0.0966 0.0348 0.8263
12.250 1.5889 0.03765 0.03108 -0.0953 0.0292 0.8276
12.500 1.5912 0.03982 0.03327 -0.0940 0.0250 0.8289
12.750 1.5952 0.04190 0.03540 -0.0929 0.0218 0.8302
13.000 1.5986 0.04411 0.03763 -0.0919 0.0191 0.8316
13.250 1.6021 0.04633 0.03990 -0.0910 0.0171 0.8331
13.500 1.6065 0.04851 0.04212 -0.0902 0.0156 0.8346
13.750 1.6109 0.05073 0.04440 -0.0895 0.0144 0.8360
14.000 1.6137 0.05318 0.04688 -0.0888 0.0132 0.8372
14.250 1.6183 0.05545 0.04921 -0.0882 0.0125 0.8384
14.500 1.6217 0.05788 0.05170 -0.0877 0.0117 0.8394
14.750 1.6240 0.06046 0.05433 -0.0871 0.0110 0.8406
15.000 1.6260 0.06309 0.05703 -0.0866 0.0103 0.8417
15.250 1.6287 0.06570 0.05972 -0.0863 0.0098 0.8429
15.500 1.6310 0.06836 0.06246 -0.0859 0.0094 0.8441
15.750 1.6321 0.07119 0.06535 -0.0856 0.0089 0.8453
16.000 1.6319 0.07421 0.06844 -0.0854 0.0085 0.8467
16.250 1.6316 0.07729 0.07159 -0.0852 0.0081 0.8481
16.500 1.6320 0.08033 0.07471 -0.0851 0.0079 0.8494
16.750 1.6322 0.08342 0.07787 -0.0851 0.0076 0.8507
17.000 1.6319 0.08656 0.08109 -0.0851 0.0073 0.8520
17.250 1.6301 0.08996 0.08458 -0.0853 0.0071 0.8531
17.500 1.6283 0.09339 0.08807 -0.0855 0.0068 0.8541
17.750 1.6256 0.09698 0.09174 -0.0858 0.0066 0.8551
18.000 1.6215 0.10081 0.09565 -0.0863 0.0064 0.8562
18.250 1.6170 0.10470 0.09963 -0.0868 0.0062 0.8573
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