HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED) (hq17-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED) (hq17-il) Reynolds number: 1,000,000 Max Cl/Cd: 122.46 at α=3° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hq17-il-1000000-n5.txt Download as CSV file: xf-hq17-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.750 -0.6149 0.03827 0.03520 -0.1527 0.8319 0.0046
-14.500 -0.6367 0.03437 0.03114 -0.1527 0.8287 0.0047
-14.250 -0.6510 0.03162 0.02821 -0.1515 0.8256 0.0045
-14.000 -0.6549 0.02973 0.02620 -0.1501 0.8228 0.0048
-13.750 -0.6538 0.02826 0.02464 -0.1485 0.8205 0.0050
-13.500 -0.6560 0.02665 0.02290 -0.1465 0.8178 0.0051
-13.250 -0.6466 0.02582 0.02203 -0.1451 0.8151 0.0053
-13.000 -0.6447 0.02457 0.02065 -0.1429 0.8120 0.0054
-12.750 -0.6335 0.02397 0.01997 -0.1413 0.8094 0.0058
-12.500 -0.6329 0.02282 0.01868 -0.1384 0.8066 0.0059
-12.250 -0.6259 0.02207 0.01783 -0.1360 0.8039 0.0061
-12.000 -0.6135 0.02128 0.01694 -0.1344 0.8014 0.0064
-11.750 -0.6007 0.02039 0.01590 -0.1328 0.7989 0.0066
-11.500 -0.5845 0.01967 0.01506 -0.1317 0.7967 0.0068
-11.250 -0.5668 0.01906 0.01434 -0.1307 0.7944 0.0071
-11.000 -0.5459 0.01863 0.01389 -0.1302 0.7921 0.0073
-10.750 -0.5234 0.01836 0.01360 -0.1298 0.7894 0.0076
-10.500 -0.4998 0.01820 0.01341 -0.1295 0.7868 0.0078
-10.250 -0.4771 0.01791 0.01308 -0.1292 0.7841 0.0081
-10.000 -0.4546 0.01757 0.01266 -0.1287 0.7815 0.0083
-9.750 -0.4315 0.01721 0.01226 -0.1284 0.7788 0.0087
-9.500 -0.4093 0.01669 0.01165 -0.1280 0.7758 0.0090
-9.250 -0.3866 0.01619 0.01106 -0.1276 0.7728 0.0093
-9.000 -0.3631 0.01579 0.01057 -0.1273 0.7700 0.0096
-8.750 -0.3383 0.01556 0.01027 -0.1272 0.7676 0.0099
-8.500 -0.3149 0.01505 0.00967 -0.1269 0.7653 0.0102
-8.250 -0.2920 0.01446 0.00901 -0.1265 0.7629 0.0105
-8.000 -0.2669 0.01424 0.00875 -0.1264 0.7604 0.0109
-7.750 -0.2416 0.01402 0.00849 -0.1263 0.7578 0.0112
-7.500 -0.2161 0.01382 0.00824 -0.1263 0.7555 0.0115
-7.250 -0.1903 0.01359 0.00798 -0.1263 0.7535 0.0120
-7.000 -0.1649 0.01319 0.00753 -0.1262 0.7513 0.0124
-6.750 -0.1393 0.01287 0.00714 -0.1262 0.7490 0.0129
-6.500 -0.1137 0.01253 0.00674 -0.1261 0.7466 0.0133
-6.250 -0.0883 0.01216 0.00631 -0.1260 0.7441 0.0136
-6.000 -0.0628 0.01183 0.00591 -0.1258 0.7419 0.0138
-5.750 -0.0367 0.01151 0.00556 -0.1258 0.7395 0.0140
-5.500 -0.0106 0.01120 0.00521 -0.1258 0.7364 0.0142
-5.250 0.0156 0.01093 0.00491 -0.1258 0.7332 0.0143
-5.000 0.0394 0.01036 0.00426 -0.1254 0.7300 0.0148
-4.750 0.0646 0.00996 0.00381 -0.1253 0.7273 0.0153
-4.500 0.0908 0.00968 0.00350 -0.1252 0.7247 0.0159
-4.250 0.1174 0.00947 0.00327 -0.1253 0.7221 0.0166
-4.000 0.1442 0.00930 0.00307 -0.1254 0.7197 0.0173
-3.750 0.1710 0.00913 0.00286 -0.1255 0.7174 0.0179
-3.500 0.1979 0.00898 0.00267 -0.1255 0.7152 0.0185
-3.250 0.2252 0.00883 0.00251 -0.1257 0.7131 0.0191
-3.000 0.2526 0.00871 0.00236 -0.1259 0.7107 0.0197
-2.750 0.2799 0.00861 0.00223 -0.1260 0.7083 0.0201
-2.500 0.3072 0.00852 0.00212 -0.1262 0.7058 0.0205
-2.250 0.3344 0.00843 0.00198 -0.1263 0.7034 0.0220
-2.000 0.3618 0.00834 0.00189 -0.1265 0.7011 0.0258
-1.750 0.3893 0.00821 0.00182 -0.1267 0.6979 0.0359
-1.500 0.4154 0.00797 0.00174 -0.1267 0.6927 0.0913
-1.250 0.4413 0.00777 0.00168 -0.1267 0.6880 0.1507
-1.000 0.4672 0.00746 0.00163 -0.1268 0.6819 0.2346
-0.750 0.4899 0.00683 0.00153 -0.1266 0.6755 0.4280
-0.500 0.5129 0.00622 0.00146 -0.1262 0.6715 0.6194
-0.250 0.5369 0.00600 0.00157 -0.1257 0.6682 0.7291
0.000 0.5635 0.00607 0.00168 -0.1255 0.6650 0.7649
0.250 0.5907 0.00615 0.00172 -0.1256 0.6620 0.7759
0.500 0.6182 0.00621 0.00181 -0.1257 0.6591 0.7837
0.750 0.6457 0.00628 0.00188 -0.1258 0.6558 0.7906
1.000 0.6725 0.00638 0.00196 -0.1258 0.6515 0.7954
1.250 0.6995 0.00646 0.00201 -0.1258 0.6470 0.7984
1.500 0.7272 0.00650 0.00205 -0.1261 0.6407 0.8008
1.750 0.7537 0.00657 0.00210 -0.1261 0.6338 0.8027
2.000 0.7797 0.00665 0.00216 -0.1259 0.6248 0.8046
2.250 0.8043 0.00676 0.00223 -0.1255 0.6149 0.8069
2.500 0.8281 0.00689 0.00231 -0.1249 0.6065 0.8092
2.750 0.8528 0.00700 0.00240 -0.1246 0.5989 0.8111
3.000 0.8756 0.00715 0.00250 -0.1238 0.5891 0.8130
3.250 0.8970 0.00734 0.00263 -0.1228 0.5766 0.8150
3.500 0.9177 0.00751 0.00276 -0.1216 0.5609 0.8166
3.750 0.9327 0.00779 0.00295 -0.1193 0.5346 0.8181
4.000 0.9339 0.00824 0.00322 -0.1141 0.4960 0.8200
4.250 0.9332 0.00887 0.00366 -0.1087 0.4579 0.8219
4.500 0.9272 0.00974 0.00427 -0.1026 0.4023 0.8241
4.750 0.9363 0.01028 0.00468 -0.0995 0.3786 0.8258
5.000 0.9443 0.01088 0.00517 -0.0963 0.3512 0.8274
5.250 0.9538 0.01148 0.00567 -0.0935 0.3309 0.8291
5.500 0.9618 0.01214 0.00623 -0.0905 0.3016 0.8309
5.750 0.9647 0.01305 0.00695 -0.0867 0.2619 0.8326
6.000 0.9695 0.01395 0.00770 -0.0834 0.2309 0.8342
6.250 0.9636 0.01537 0.00881 -0.0786 0.1690 0.8361
6.500 0.9660 0.01651 0.00976 -0.0752 0.1300 0.8379
6.750 0.9594 0.01816 0.01107 -0.0707 0.0651 0.8399
7.000 0.9764 0.01868 0.01160 -0.0696 0.0617 0.8411
7.250 0.9932 0.01923 0.01213 -0.0685 0.0573 0.8422
7.500 1.0110 0.01972 0.01264 -0.0675 0.0549 0.8431
7.750 1.0238 0.02048 0.01336 -0.0659 0.0422 0.8441
8.000 1.0379 0.02118 0.01404 -0.0645 0.0340 0.8453
8.250 1.0467 0.02222 0.01500 -0.0624 0.0163 0.8465
8.500 1.0615 0.02293 0.01572 -0.0612 0.0120 0.8477
8.750 1.0726 0.02389 0.01666 -0.0596 0.0040 0.8489
9.000 1.0881 0.02459 0.01740 -0.0585 0.0038 0.8503
9.250 1.1030 0.02536 0.01819 -0.0574 0.0035 0.8516
9.500 1.1174 0.02618 0.01905 -0.0563 0.0030 0.8527
9.750 1.1316 0.02702 0.01993 -0.0552 0.0028 0.8538
10.000 1.1462 0.02786 0.02081 -0.0542 0.0028 0.8548
10.250 1.1602 0.02876 0.02175 -0.0532 0.0027 0.8557
10.500 1.1738 0.02969 0.02272 -0.0521 0.0025 0.8565
10.750 1.1872 0.03064 0.02372 -0.0511 0.0025 0.8574
11.000 1.1990 0.03173 0.02486 -0.0499 0.0022 0.8583
11.250 1.2118 0.03277 0.02595 -0.0489 0.0023 0.8593
11.500 1.2230 0.03395 0.02719 -0.0478 0.0022 0.8604
11.750 1.2341 0.03518 0.02848 -0.0467 0.0021 0.8614
12.000 1.2452 0.03642 0.02978 -0.0457 0.0021 0.8624
12.250 1.2557 0.03773 0.03114 -0.0447 0.0020 0.8633
12.500 1.2655 0.03913 0.03260 -0.0438 0.0019 0.8643
12.750 1.2744 0.04065 0.03418 -0.0427 0.0018 0.8652
13.000 1.2825 0.04227 0.03586 -0.0418 0.0017 0.8661
13.250 1.2897 0.04400 0.03766 -0.0408 0.0017 0.8669
13.500 1.3003 0.04545 0.03915 -0.0402 0.0017 0.8677
13.750 1.2980 0.04821 0.04203 -0.0387 0.0016 0.8685
14.000 1.3022 0.05039 0.04428 -0.0378 0.0015 0.8691
14.250 1.3075 0.05250 0.04648 -0.0371 0.0015 0.8698
14.500 1.3085 0.05509 0.04917 -0.0363 0.0015 0.8706
14.750 1.3142 0.05725 0.05141 -0.0358 0.0015 0.8714
15.000 1.3178 0.05970 0.05394 -0.0353 0.0015 0.8722
15.250 1.3199 0.06238 0.05672 -0.0349 0.0015 0.8729
15.500 1.3259 0.06465 0.05907 -0.0347 0.0015 0.8737
15.750 1.3278 0.06745 0.06196 -0.0345 0.0015 0.8744
16.000 1.3349 0.06967 0.06426 -0.0346 0.0014 0.8753
16.250 1.3353 0.07278 0.06746 -0.0346 0.0014 0.8760
16.500 1.3354 0.07603 0.07081 -0.0347 0.0014 0.8767
16.750 1.3388 0.07888 0.07375 -0.0350 0.0014 0.8774
17.000 1.3389 0.08223 0.07719 -0.0354 0.0014 0.8781
17.250 1.3403 0.08547 0.08054 -0.0359 0.0014 0.8788
17.500 1.3386 0.08922 0.08440 -0.0365 0.0014 0.8795
17.750 1.3350 0.09334 0.08863 -0.0374 0.0013 0.8801
18.000 1.3337 0.09718 0.09257 -0.0384 0.0013 0.8807
18.250 1.3306 0.10134 0.09684 -0.0395 0.0013 0.8813
18.500 1.3302 0.10516 0.10076 -0.0408 0.0013 0.8819
18.750 1.3241 0.10996 0.10568 -0.0424 0.0013 0.8824
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