HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| 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: 139.79 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hq300gd2-il-1000000.txt Download as CSV file: xf-hq300gd2-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.250 -0.6394 0.05459 0.05232 -0.0817 0.8857 0.0103
-13.000 -0.6919 0.04404 0.04131 -0.0883 0.8659 0.0103
-12.750 -0.7192 0.03839 0.03529 -0.0897 0.8500 0.0103
-12.500 -0.7324 0.03460 0.03119 -0.0896 0.8367 0.0104
-12.250 -0.7361 0.03185 0.02816 -0.0890 0.8250 0.0105
-12.000 -0.7327 0.02981 0.02589 -0.0883 0.8144 0.0106
-11.750 -0.7257 0.02822 0.02410 -0.0876 0.8050 0.0107
-11.500 -0.7190 0.02565 0.02119 -0.0874 0.7959 0.0109
-11.250 -0.7078 0.02337 0.01867 -0.0872 0.7880 0.0113
-11.000 -0.6865 0.02261 0.01780 -0.0873 0.7802 0.0115
-10.750 -0.6634 0.02202 0.01715 -0.0875 0.7733 0.0117
-10.500 -0.6396 0.02147 0.01651 -0.0877 0.7664 0.0120
-10.250 -0.6157 0.02085 0.01579 -0.0878 0.7601 0.0123
-10.000 -0.5915 0.02012 0.01495 -0.0880 0.7538 0.0126
-9.750 -0.5671 0.01942 0.01411 -0.0881 0.7475 0.0130
-9.500 -0.5418 0.01875 0.01332 -0.0883 0.7419 0.0134
-9.250 -0.5153 0.01835 0.01281 -0.0886 0.7361 0.0137
-9.000 -0.4921 0.01708 0.01138 -0.0886 0.7308 0.0143
-8.750 -0.4658 0.01656 0.01082 -0.0890 0.7260 0.0147
-8.500 -0.4384 0.01620 0.01043 -0.0894 0.7209 0.0152
-8.250 -0.4111 0.01580 0.00996 -0.0897 0.7158 0.0157
-8.000 -0.3838 0.01536 0.00945 -0.0901 0.7111 0.0163
-7.750 -0.3559 0.01493 0.00896 -0.0905 0.7065 0.0168
-7.500 -0.3277 0.01464 0.00859 -0.0909 0.7019 0.0173
-7.250 -0.3018 0.01373 0.00757 -0.0911 0.6976 0.0181
-7.000 -0.2737 0.01327 0.00711 -0.0916 0.6938 0.0188
-6.750 -0.2448 0.01300 0.00683 -0.0922 0.6896 0.0196
-6.500 -0.2160 0.01275 0.00653 -0.0927 0.6853 0.0205
-6.250 -0.1871 0.01250 0.00622 -0.0932 0.6810 0.0212
-6.000 -0.1576 0.01227 0.00596 -0.0938 0.6776 0.0217
-5.750 -0.1286 0.01149 0.00513 -0.0946 0.6740 0.0230
-5.500 -0.0989 0.01119 0.00482 -0.0954 0.6703 0.0240
-5.250 -0.0691 0.01100 0.00459 -0.0961 0.6665 0.0251
-5.000 -0.0390 0.01080 0.00435 -0.0968 0.6630 0.0263
-4.750 -0.0085 0.01059 0.00413 -0.0976 0.6596 0.0270
-4.500 0.0226 0.01018 0.00367 -0.0986 0.6563 0.0287
-4.250 0.0532 0.00999 0.00346 -0.0995 0.6530 0.0306
-4.000 0.0837 0.00986 0.00329 -0.1003 0.6493 0.0324
-3.750 0.1148 0.00968 0.00310 -0.1012 0.6464 0.0342
-3.500 0.1462 0.00946 0.00290 -0.1022 0.6432 0.0390
-3.250 0.1775 0.00927 0.00274 -0.1032 0.6400 0.0485
-3.000 0.2095 0.00902 0.00259 -0.1044 0.6369 0.0781
-2.750 0.2456 0.00832 0.00237 -0.1072 0.6334 0.2282
-2.500 0.2855 0.00749 0.00218 -0.1109 0.6307 0.4181
-2.250 0.3278 0.00674 0.00204 -0.1151 0.6276 0.6041
-2.000 0.3616 0.00659 0.00211 -0.1165 0.6245 0.6846
-1.750 0.3925 0.00664 0.00217 -0.1172 0.6214 0.7109
-1.500 0.4228 0.00676 0.00224 -0.1178 0.6179 0.7283
-1.250 0.4529 0.00685 0.00235 -0.1182 0.6152 0.7425
-1.000 0.4819 0.00696 0.00248 -0.1184 0.6123 0.7530
-0.750 0.5126 0.00706 0.00253 -0.1191 0.6092 0.7596
-0.500 0.5417 0.00713 0.00259 -0.1194 0.6059 0.7636
-0.250 0.5710 0.00724 0.00265 -0.1198 0.6022 0.7665
0.000 0.6010 0.00729 0.00270 -0.1203 0.5990 0.7696
0.250 0.6313 0.00733 0.00273 -0.1209 0.5952 0.7728
0.500 0.6618 0.00740 0.00276 -0.1217 0.5913 0.7757
0.750 0.6907 0.00748 0.00281 -0.1220 0.5873 0.7786
1.000 0.7193 0.00757 0.00292 -0.1222 0.5838 0.7819
1.250 0.7484 0.00765 0.00302 -0.1225 0.5802 0.7856
1.500 0.7782 0.00773 0.00308 -0.1230 0.5765 0.7888
1.750 0.8082 0.00782 0.00313 -0.1237 0.5727 0.7910
2.000 0.8381 0.00788 0.00318 -0.1243 0.5690 0.7929
2.250 0.8676 0.00790 0.00322 -0.1248 0.5654 0.7946
2.500 0.8967 0.00795 0.00329 -0.1252 0.5614 0.7961
2.750 0.9256 0.00803 0.00336 -0.1256 0.5574 0.7977
3.000 0.9547 0.00812 0.00344 -0.1261 0.5534 0.7994
3.250 0.9844 0.00816 0.00352 -0.1266 0.5491 0.8010
3.500 1.0137 0.00824 0.00359 -0.1272 0.5444 0.8028
3.750 1.0427 0.00836 0.00367 -0.1277 0.5393 0.8046
4.000 1.0727 0.00840 0.00375 -0.1283 0.5346 0.8062
4.250 1.1021 0.00848 0.00383 -0.1289 0.5288 0.8077
4.500 1.1308 0.00858 0.00391 -0.1294 0.5230 0.8092
4.750 1.1596 0.00863 0.00400 -0.1298 0.5168 0.8106
5.000 1.1874 0.00875 0.00411 -0.1301 0.5096 0.8119
5.250 1.2158 0.00884 0.00423 -0.1304 0.5023 0.8132
5.500 1.2432 0.00900 0.00437 -0.1306 0.4938 0.8147
5.750 1.2713 0.00911 0.00451 -0.1309 0.4845 0.8163
6.000 1.2986 0.00929 0.00467 -0.1312 0.4740 0.8178
6.250 1.3255 0.00949 0.00485 -0.1313 0.4617 0.8193
6.500 1.3520 0.00973 0.00505 -0.1315 0.4476 0.8208
6.750 1.3780 0.01001 0.00527 -0.1315 0.4313 0.8224
7.000 1.4033 0.01033 0.00554 -0.1314 0.4133 0.8238
7.250 1.4273 0.01068 0.00583 -0.1312 0.3940 0.8253
7.500 1.4498 0.01110 0.00618 -0.1306 0.3743 0.8266
7.750 1.4714 0.01156 0.00656 -0.1299 0.3547 0.8279
8.000 1.4916 0.01208 0.00701 -0.1290 0.3319 0.8293
8.250 1.5090 0.01274 0.00753 -0.1276 0.3062 0.8308
8.500 1.5241 0.01348 0.00813 -0.1259 0.2800 0.8326
8.750 1.5417 0.01404 0.00863 -0.1245 0.2629 0.8344
9.000 1.5583 0.01460 0.00915 -0.1231 0.2485 0.8361
9.250 1.5696 0.01521 0.00971 -0.1206 0.2345 0.8378
9.500 1.5793 0.01593 0.01038 -0.1180 0.2202 0.8393
9.750 1.5908 0.01673 0.01114 -0.1160 0.2062 0.8410
10.000 1.6007 0.01763 0.01202 -0.1139 0.1924 0.8428
10.250 1.6087 0.01873 0.01307 -0.1117 0.1781 0.8446
10.500 1.6155 0.02000 0.01430 -0.1096 0.1635 0.8463
11.000 1.6266 0.02300 0.01721 -0.1057 0.1352 0.8498
11.250 1.6310 0.02471 0.01888 -0.1040 0.1220 0.8515
11.500 1.6343 0.02657 0.02069 -0.1023 0.1089 0.8531
11.750 1.6365 0.02858 0.02265 -0.1006 0.0964 0.8546
12.000 1.6377 0.03071 0.02475 -0.0989 0.0845 0.8562
12.250 1.6367 0.03302 0.02702 -0.0972 0.0725 0.8579
12.500 1.6353 0.03542 0.02940 -0.0955 0.0618 0.8593
12.750 1.6331 0.03794 0.03190 -0.0939 0.0518 0.8607
13.000 1.6303 0.04057 0.03451 -0.0923 0.0431 0.8622
13.250 1.6281 0.04326 0.03719 -0.0910 0.0357 0.8636
13.500 1.6263 0.04598 0.03992 -0.0898 0.0298 0.8651
13.750 1.6249 0.04873 0.04268 -0.0888 0.0252 0.8665
14.000 1.6259 0.05130 0.04528 -0.0879 0.0221 0.8680
14.250 1.6264 0.05400 0.04802 -0.0872 0.0197 0.8693
14.500 1.6273 0.05668 0.05075 -0.0865 0.0181 0.8706
14.750 1.6258 0.05965 0.05377 -0.0858 0.0164 0.8720
15.000 1.6290 0.06214 0.05634 -0.0853 0.0156 0.8733
15.250 1.6295 0.06497 0.05924 -0.0849 0.0146 0.8746
15.500 1.6286 0.06801 0.06233 -0.0845 0.0138 0.8759
15.750 1.6261 0.07125 0.06565 -0.0841 0.0130 0.8772
16.000 1.6273 0.07413 0.06861 -0.0839 0.0125 0.8786
16.250 1.6277 0.07713 0.07169 -0.0837 0.0120 0.8799
16.500 1.6260 0.08045 0.07508 -0.0837 0.0115 0.8813
16.750 1.6224 0.08406 0.07875 -0.0837 0.0110 0.8826
17.000 1.6147 0.08821 0.08299 -0.0838 0.0105 0.8837
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