HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED) (hq17-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED) (hq17-il) Reynolds number: 500,000 Max Cl/Cd: 103.3 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hq17-il-500000-n5.txt Download as CSV file: xf-hq17-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURE
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
------ -------- --------- --------- -------- -------- --------
-11.500 -0.0791 0.08685 0.08353 -0.1308 0.8347 0.0079
-11.250 -0.0804 0.08289 0.07961 -0.1324 0.8320 0.0085
-11.000 -0.0872 0.07791 0.07466 -0.1343 0.8290 0.0089
-10.750 -0.1050 0.07107 0.06787 -0.1370 0.8257 0.0091
-9.750 -0.3467 0.02918 0.02479 -0.1374 0.8062 0.0100
-9.500 -0.3442 0.02723 0.02263 -0.1352 0.8027 0.0103
-9.250 -0.3282 0.02659 0.02192 -0.1343 0.7999 0.0105
-9.000 -0.3106 0.02603 0.02124 -0.1335 0.7976 0.0107
-8.750 -0.2934 0.02521 0.02027 -0.1327 0.7955 0.0110
-8.500 -0.2759 0.02425 0.01917 -0.1319 0.7932 0.0114
-8.250 -0.2567 0.02348 0.01827 -0.1312 0.7903 0.0120
-8.000 -0.2381 0.02235 0.01694 -0.1304 0.7873 0.0127
-7.750 -0.2182 0.02125 0.01563 -0.1296 0.7845 0.0134
-7.500 -0.1968 0.02027 0.01442 -0.1290 0.7819 0.0138
-7.250 -0.1746 0.01940 0.01337 -0.1285 0.7793 0.0141
-7.000 -0.1538 0.01795 0.01169 -0.1279 0.7766 0.0147
-6.750 -0.1310 0.01705 0.01071 -0.1276 0.7739 0.0154
-6.500 -0.1067 0.01645 0.01004 -0.1274 0.7714 0.0159
-6.250 -0.0821 0.01583 0.00931 -0.1271 0.7693 0.0164
-6.000 -0.0572 0.01522 0.00862 -0.1269 0.7672 0.0168
-5.750 -0.0324 0.01467 0.00799 -0.1267 0.7647 0.0173
-5.500 -0.0075 0.01413 0.00737 -0.1265 0.7624 0.0178
-5.250 0.0176 0.01364 0.00681 -0.1262 0.7601 0.0183
-5.000 0.0427 0.01319 0.00629 -0.1260 0.7580 0.0188
-4.750 0.0683 0.01283 0.00585 -0.1259 0.7559 0.0194
-4.500 0.0939 0.01252 0.00550 -0.1258 0.7535 0.0200
-4.250 0.1192 0.01221 0.00515 -0.1256 0.7507 0.0204
-4.000 0.1442 0.01184 0.00474 -0.1254 0.7482 0.0208
-3.750 0.1689 0.01140 0.00424 -0.1251 0.7458 0.0217
-3.500 0.1948 0.01112 0.00391 -0.1250 0.7436 0.0227
-3.250 0.2216 0.01091 0.00364 -0.1251 0.7416 0.0239
-3.000 0.2476 0.01073 0.00346 -0.1251 0.7387 0.0251
-2.750 0.2740 0.01057 0.00329 -0.1251 0.7356 0.0265
-2.500 0.3008 0.01045 0.00314 -0.1251 0.7327 0.0287
-2.250 0.3276 0.01028 0.00296 -0.1252 0.7299 0.0353
-2.000 0.3535 0.01000 0.00281 -0.1252 0.7272 0.0757
-1.750 0.3789 0.00969 0.00273 -0.1252 0.7245 0.1467
-1.500 0.4039 0.00930 0.00264 -0.1252 0.7219 0.2413
-1.250 0.4223 0.00804 0.00245 -0.1246 0.7194 0.5800
-1.000 0.4450 0.00776 0.00261 -0.1236 0.7170 0.7089
-0.750 0.4708 0.00791 0.00284 -0.1231 0.7145 0.7643
-0.500 0.4966 0.00811 0.00305 -0.1226 0.7116 0.7865
-0.250 0.5235 0.00822 0.00313 -0.1225 0.7084 0.7928
0.000 0.5511 0.00834 0.00319 -0.1225 0.7051 0.8014
0.250 0.5778 0.00849 0.00330 -0.1223 0.7015 0.8076
0.500 0.6034 0.00857 0.00337 -0.1221 0.6959 0.8129
0.750 0.6303 0.00861 0.00336 -0.1221 0.6903 0.8159
1.000 0.6561 0.00866 0.00342 -0.1219 0.6851 0.8178
1.250 0.6822 0.00872 0.00346 -0.1217 0.6804 0.8199
1.500 0.7089 0.00877 0.00349 -0.1217 0.6767 0.8220
1.750 0.7357 0.00883 0.00354 -0.1218 0.6734 0.8242
2.000 0.7624 0.00888 0.00358 -0.1218 0.6698 0.8265
2.250 0.7891 0.00893 0.00359 -0.1219 0.6655 0.8288
2.500 0.8150 0.00899 0.00363 -0.1218 0.6612 0.8301
2.750 0.8398 0.00906 0.00374 -0.1214 0.6559 0.8316
3.000 0.8649 0.00914 0.00381 -0.1211 0.6509 0.8330
3.250 0.8895 0.00921 0.00389 -0.1207 0.6451 0.8345
3.500 0.9132 0.00929 0.00399 -0.1202 0.6378 0.8363
3.750 0.9366 0.00936 0.00409 -0.1196 0.6299 0.8382
4.000 0.9596 0.00945 0.00417 -0.1189 0.6222 0.8399
4.250 0.9818 0.00955 0.00425 -0.1181 0.6135 0.8416
4.500 1.0010 0.00969 0.00435 -0.1166 0.6028 0.8432
4.750 1.0170 0.00986 0.00449 -0.1145 0.5916 0.8446
5.000 1.0302 0.01005 0.00466 -0.1117 0.5788 0.8463
5.250 1.0410 0.01030 0.00488 -0.1086 0.5603 0.8482
5.500 1.0457 0.01073 0.00522 -0.1044 0.5320 0.8506
5.750 1.0491 0.01128 0.00564 -0.1002 0.5056 0.8530
6.000 1.0483 0.01204 0.00625 -0.0954 0.4736 0.8552
6.250 1.0450 0.01298 0.00702 -0.0904 0.4396 0.8574
6.500 1.0430 0.01397 0.00786 -0.0858 0.3987 0.8594
6.750 1.0325 0.01543 0.00906 -0.0802 0.3498 0.8617
7.000 1.0351 0.01649 0.00998 -0.0768 0.3218 0.8638
7.250 1.0278 0.01809 0.01127 -0.0722 0.2640 0.8659
7.500 1.0258 0.01955 0.01249 -0.0685 0.2210 0.8677
7.750 1.0196 0.02133 0.01392 -0.0645 0.1595 0.8694
8.000 1.0236 0.02258 0.01501 -0.0619 0.1279 0.8710
8.250 1.0270 0.02391 0.01616 -0.0593 0.0915 0.8725
8.750 1.0472 0.02596 0.01811 -0.0560 0.0617 0.8752
9.000 1.0619 0.02673 0.01890 -0.0549 0.0581 0.8766
9.500 1.0833 0.02889 0.02097 -0.0521 0.0264 0.8796
9.750 1.0905 0.03029 0.02229 -0.0504 0.0147 0.8809
10.000 1.1030 0.03133 0.02334 -0.0493 0.0067 0.8820
10.250 1.1134 0.03255 0.02458 -0.0480 0.0051 0.8831
10.500 1.1264 0.03357 0.02565 -0.0471 0.0045 0.8843
10.750 1.1396 0.03461 0.02675 -0.0461 0.0044 0.8855
11.000 1.1515 0.03578 0.02801 -0.0451 0.0040 0.8867
11.250 1.1640 0.03692 0.02921 -0.0443 0.0039 0.8881
11.500 1.1755 0.03816 0.03054 -0.0433 0.0038 0.8896
11.750 1.1861 0.03952 0.03199 -0.0424 0.0035 0.8910
12.000 1.1975 0.04084 0.03339 -0.0416 0.0035 0.8923
12.250 1.2070 0.04235 0.03500 -0.0407 0.0034 0.8935
12.500 1.2158 0.04397 0.03670 -0.0398 0.0033 0.8948
12.750 1.2233 0.04574 0.03857 -0.0389 0.0031 0.8959
13.250 1.2366 0.04958 0.04260 -0.0373 0.0030 0.8984
13.500 1.2465 0.05123 0.04433 -0.0368 0.0031 0.8998
13.750 1.2442 0.05421 0.04744 -0.0357 0.0029 0.9012
14.000 1.2479 0.05661 0.04994 -0.0351 0.0029 0.9026
14.250 1.2523 0.05901 0.05244 -0.0347 0.0028 0.9042
14.500 1.2549 0.06169 0.05523 -0.0343 0.0028 0.9057
14.750 1.2608 0.06409 0.05774 -0.0341 0.0028 0.9074
15.000 1.2648 0.06674 0.06049 -0.0341 0.0027 0.9091
15.500 1.2733 0.07223 0.06620 -0.0343 0.0026 0.9133
15.750 1.2759 0.07529 0.06938 -0.0346 0.0026 0.9160
16.000 1.2823 0.07794 0.07215 -0.0351 0.0025 0.9196
16.250 1.2841 0.08126 0.07560 -0.0356 0.0025 0.9231
16.750 1.2883 0.08863 0.08325 -0.0379 0.0024 0.9383
17.000 1.2878 0.09229 0.08704 -0.0389 0.0023 0.9878
17.250 1.2848 0.09573 0.09058 -0.0389 0.0023 1.0000
17.500 1.2834 0.09954 0.09451 -0.0398 0.0023 1.0000
17.750 1.2810 0.10356 0.09865 -0.0408 0.0023 1.0000
18.000 1.2789 0.10762 0.10284 -0.0420 0.0023 1.0000
18.250 1.2763 0.11180 0.10714 -0.0433 0.0022 1.0000
18.500 1.2741 0.11599 0.11145 -0.0449 0.0022 1.0000
18.750 1.2703 0.12045 0.11604 -0.0465 0.0022 1.0000
19.000 1.2669 0.12493 0.12064 -0.0484 0.0022 1.0000
19.250 1.2629 0.12956 0.12540 -0.0504 0.0022 1.0000
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