AH 93-W-215 (ah93w215-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: AH 93-W-215 (ah93w215-il) Reynolds number: 1,000,000 Max Cl/Cd: 97.35 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w215-il-1000000-n5.txt Download as CSV file: xf-ah93w215-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-215
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1266 0.07523 0.07113 -0.0695 1.0000 0.0276
-19.500 -1.1376 0.07065 0.06646 -0.0715 1.0000 0.0279
-19.250 -1.1460 0.06651 0.06224 -0.0732 1.0000 0.0282
-19.000 -1.1462 0.06249 0.05814 -0.0761 0.9996 0.0286
-18.750 -1.1384 0.05868 0.05425 -0.0800 0.9986 0.0291
-18.500 -1.1272 0.05510 0.05059 -0.0842 0.9968 0.0294
-18.250 -1.1163 0.05222 0.04763 -0.0869 0.9945 0.0300
-18.000 -1.1178 0.04909 0.04444 -0.0878 0.9917 0.0304
-17.750 -1.1177 0.04624 0.04154 -0.0886 0.9881 0.0309
-17.500 -1.0853 0.04296 0.03817 -0.0957 0.9290 0.0316
-17.250 -1.0118 0.04010 0.03469 -0.1104 0.7939 0.0329
-17.000 -1.0028 0.03838 0.03279 -0.1112 0.7599 0.0334
-16.750 -0.9935 0.03670 0.03098 -0.1118 0.7403 0.0339
-16.500 -0.9847 0.03499 0.02914 -0.1124 0.7247 0.0342
-16.250 -0.9764 0.03329 0.02737 -0.1129 0.7132 0.0352
-16.000 -0.9662 0.03179 0.02580 -0.1133 0.7035 0.0358
-15.750 -0.9553 0.03040 0.02433 -0.1136 0.6956 0.0365
-15.500 -0.9426 0.02913 0.02299 -0.1139 0.6884 0.0373
-15.250 -0.9294 0.02795 0.02175 -0.1141 0.6828 0.0378
-15.000 -0.9145 0.02689 0.02062 -0.1143 0.6769 0.0383
-14.750 -0.9010 0.02572 0.01940 -0.1145 0.6710 0.0394
-14.500 -0.8861 0.02467 0.01830 -0.1147 0.6664 0.0402
-14.250 -0.8698 0.02372 0.01732 -0.1149 0.6619 0.0411
-14.000 -0.8524 0.02283 0.01638 -0.1152 0.6571 0.0421
-13.750 -0.8321 0.02207 0.01555 -0.1157 0.6513 0.0429
-13.500 -0.8118 0.02128 0.01471 -0.1163 0.6471 0.0439
-13.250 -0.7923 0.02047 0.01388 -0.1167 0.6440 0.0451
-13.000 -0.7719 0.01979 0.01317 -0.1170 0.6404 0.0463
-12.750 -0.7523 0.01915 0.01249 -0.1170 0.6368 0.0472
-12.500 -0.7319 0.01861 0.01190 -0.1170 0.6332 0.0484
-12.250 -0.7133 0.01800 0.01125 -0.1167 0.6295 0.0498
-12.000 -0.6947 0.01744 0.01068 -0.1163 0.6264 0.0512
-11.750 -0.6759 0.01694 0.01016 -0.1158 0.6237 0.0527
-11.500 -0.6566 0.01649 0.00968 -0.1152 0.6204 0.0538
-11.250 -0.6383 0.01603 0.00919 -0.1144 0.6170 0.0553
-11.000 -0.6205 0.01559 0.00874 -0.1135 0.6139 0.0573
-10.750 -0.6020 0.01522 0.00833 -0.1125 0.6109 0.0587
-10.250 -0.5667 0.01449 0.00757 -0.1101 0.6059 0.0624
-10.000 -0.5495 0.01415 0.00723 -0.1087 0.6036 0.0644
-9.750 -0.5321 0.01385 0.00691 -0.1072 0.6007 0.0664
-9.500 -0.5157 0.01355 0.00660 -0.1054 0.5978 0.0685
-9.250 -0.5004 0.01325 0.00629 -0.1035 0.5951 0.0711
-9.000 -0.4840 0.01302 0.00604 -0.1015 0.5925 0.0733
-8.750 -0.4681 0.01280 0.00580 -0.0994 0.5899 0.0756
-8.500 -0.4537 0.01259 0.00558 -0.0970 0.5876 0.0780
-8.250 -0.4388 0.01242 0.00541 -0.0946 0.5858 0.0805
-8.000 -0.4204 0.01225 0.00524 -0.0929 0.5836 0.0831
-7.750 -0.4019 0.01203 0.00504 -0.0912 0.5811 0.0868
-7.500 -0.3817 0.01186 0.00486 -0.0898 0.5786 0.0903
-7.250 -0.3610 0.01170 0.00469 -0.0885 0.5761 0.0934
-7.000 -0.3407 0.01152 0.00452 -0.0871 0.5738 0.0981
-6.750 -0.3190 0.01138 0.00437 -0.0860 0.5713 0.1020
-6.500 -0.2980 0.01121 0.00421 -0.0847 0.5686 0.1070
-6.250 -0.2750 0.01106 0.00407 -0.0837 0.5669 0.1116
-6.000 -0.2529 0.01088 0.00392 -0.0827 0.5648 0.1178
-5.750 -0.2295 0.01074 0.00379 -0.0818 0.5627 0.1231
-5.500 -0.2065 0.01059 0.00366 -0.0809 0.5604 0.1290
-5.250 -0.1832 0.01045 0.00354 -0.0800 0.5579 0.1357
-5.000 -0.1604 0.01031 0.00341 -0.0790 0.5551 0.1438
-4.500 -0.1138 0.01006 0.00319 -0.0773 0.5500 0.1603
-4.250 -0.0891 0.00993 0.00310 -0.0766 0.5484 0.1686
-4.000 -0.0650 0.00979 0.00299 -0.0759 0.5463 0.1793
-3.750 -0.0412 0.00963 0.00289 -0.0751 0.5438 0.1922
-3.500 -0.0171 0.00950 0.00280 -0.0744 0.5414 0.2047
-3.250 0.0070 0.00937 0.00271 -0.0736 0.5390 0.2182
-3.000 0.0304 0.00923 0.00262 -0.0728 0.5364 0.2352
-2.750 0.0537 0.00910 0.00254 -0.0718 0.5337 0.2536
-2.500 0.0769 0.00895 0.00246 -0.0709 0.5311 0.2751
-2.250 0.1003 0.00876 0.00238 -0.0701 0.5292 0.3021
-2.000 0.1238 0.00859 0.00230 -0.0692 0.5269 0.3295
-1.750 0.1467 0.00841 0.00224 -0.0682 0.5243 0.3616
-1.500 0.1700 0.00827 0.00219 -0.0673 0.5214 0.3895
-1.250 0.1934 0.00816 0.00215 -0.0664 0.5186 0.4155
-1.000 0.2173 0.00810 0.00213 -0.0656 0.5156 0.4352
-0.750 0.2417 0.00804 0.00212 -0.0648 0.5128 0.4526
-0.500 0.2671 0.00798 0.00211 -0.0643 0.5108 0.4692
-0.250 0.2928 0.00795 0.00211 -0.0638 0.5079 0.4832
0.000 0.3179 0.00792 0.00211 -0.0632 0.5048 0.4952
0.250 0.3431 0.00791 0.00211 -0.0626 0.5019 0.5057
0.500 0.3675 0.00791 0.00212 -0.0618 0.4987 0.5176
0.750 0.3917 0.00792 0.00214 -0.0610 0.4955 0.5273
1.000 0.4173 0.00790 0.00216 -0.0605 0.4929 0.5391
1.250 0.4423 0.00789 0.00219 -0.0599 0.4899 0.5498
1.500 0.4670 0.00790 0.00221 -0.0592 0.4865 0.5622
1.750 0.4897 0.00789 0.00224 -0.0581 0.4829 0.5762
2.000 0.5116 0.00792 0.00227 -0.0568 0.4790 0.5866
2.250 0.5349 0.00792 0.00231 -0.0558 0.4761 0.5958
2.500 0.5591 0.00794 0.00234 -0.0550 0.4725 0.6029
2.750 0.5817 0.00795 0.00238 -0.0539 0.4686 0.6104
3.000 0.6037 0.00799 0.00243 -0.0526 0.4643 0.6180
3.250 0.6256 0.00806 0.00248 -0.0514 0.4602 0.6244
3.500 0.6489 0.00808 0.00254 -0.0505 0.4568 0.6326
3.750 0.6719 0.00813 0.00261 -0.0495 0.4522 0.6404
4.000 0.6938 0.00820 0.00269 -0.0482 0.4477 0.6481
4.250 0.7140 0.00829 0.00279 -0.0467 0.4428 0.6572
4.500 0.7375 0.00835 0.00287 -0.0458 0.4392 0.6653
4.750 0.7587 0.00842 0.00297 -0.0445 0.4337 0.6742
5.000 0.7780 0.00854 0.00309 -0.0428 0.4282 0.6835
5.250 0.7982 0.00864 0.00321 -0.0413 0.4236 0.6925
5.500 0.8192 0.00872 0.00333 -0.0400 0.4186 0.7032
5.750 0.8385 0.00885 0.00347 -0.0383 0.4130 0.7122
6.000 0.8571 0.00899 0.00362 -0.0366 0.4077 0.7233
6.250 0.8777 0.00909 0.00376 -0.0352 0.4025 0.7338
6.500 0.8955 0.00925 0.00394 -0.0333 0.3954 0.7454
6.750 0.9128 0.00942 0.00412 -0.0314 0.3900 0.7558
7.000 0.9316 0.00957 0.00430 -0.0298 0.3835 0.7677
7.250 0.9481 0.00977 0.00453 -0.0278 0.3769 0.7782
7.500 0.9662 0.00996 0.00474 -0.0261 0.3715 0.7904
7.750 0.9837 0.01017 0.00498 -0.0243 0.3644 0.8013
8.000 0.9994 0.01046 0.00527 -0.0224 0.3579 0.8129
8.250 1.0191 0.01066 0.00553 -0.0212 0.3525 0.8244
8.500 1.0373 0.01096 0.00584 -0.0198 0.3454 0.8348
8.750 1.0556 0.01132 0.00622 -0.0186 0.3383 0.8460
9.000 1.0768 0.01167 0.00659 -0.0181 0.3301 0.8562
9.250 1.0981 0.01215 0.00708 -0.0178 0.3216 0.8681
9.500 1.1262 0.01259 0.00755 -0.0189 0.3131 0.8792
9.750 1.1545 0.01314 0.00811 -0.0203 0.3060 0.8900
10.000 1.1900 0.01361 0.00862 -0.0230 0.2988 0.9000
10.250 1.2252 0.01437 0.00937 -0.0262 0.2880 0.9093
10.500 1.2564 0.01514 0.01016 -0.0287 0.2776 0.9216
10.750 1.2876 0.01595 0.01099 -0.0312 0.2684 0.9374
11.000 1.3202 0.01704 0.01208 -0.0346 0.2575 0.9577
11.500 1.3460 0.01976 0.01477 -0.0339 0.2383 1.0000
11.750 1.3503 0.02139 0.01638 -0.0325 0.2284 1.0000
12.000 1.3578 0.02285 0.01784 -0.0315 0.2212 1.0000
12.250 1.3606 0.02466 0.01964 -0.0303 0.2124 1.0000
12.500 1.3666 0.02627 0.02125 -0.0293 0.2058 1.0000
12.750 1.3707 0.02803 0.02301 -0.0283 0.1992 1.0000
13.000 1.3717 0.03001 0.02498 -0.0271 0.1910 1.0000
13.250 1.3744 0.03188 0.02685 -0.0260 0.1844 1.0000
13.500 1.3761 0.03386 0.02882 -0.0250 0.1775 1.0000
13.750 1.3777 0.03589 0.03086 -0.0240 0.1711 1.0000
14.000 1.3785 0.03802 0.03298 -0.0231 0.1640 1.0000
14.250 1.3799 0.04017 0.03513 -0.0223 0.1573 1.0000
14.500 1.3801 0.04246 0.03741 -0.0215 0.1506 1.0000
14.750 1.3800 0.04479 0.03973 -0.0208 0.1431 1.0000
15.000 1.3813 0.04708 0.04203 -0.0202 0.1371 1.0000
15.250 1.3825 0.04940 0.04434 -0.0197 0.1308 1.0000
15.500 1.3826 0.05186 0.04680 -0.0192 0.1246 1.0000
15.750 1.3824 0.05436 0.04929 -0.0187 0.1182 1.0000
16.000 1.3824 0.05692 0.05185 -0.0184 0.1122 1.0000
16.250 1.3830 0.05944 0.05437 -0.0181 0.1072 1.0000
16.500 1.3829 0.06205 0.05699 -0.0178 0.1014 1.0000
16.750 1.3817 0.06482 0.05976 -0.0176 0.0962 1.0000
17.000 1.3831 0.06735 0.06230 -0.0176 0.0916 1.0000
17.250 1.3781 0.07062 0.06556 -0.0175 0.0849 1.0000
17.500 1.3792 0.07324 0.06819 -0.0175 0.0807 1.0000
17.750 1.3763 0.07634 0.07130 -0.0176 0.0765 1.0000
18.000 1.3797 0.07876 0.07375 -0.0177 0.0741 1.0000
18.250 1.3753 0.08214 0.07715 -0.0179 0.0699 1.0000
18.500 1.3762 0.08490 0.07993 -0.0182 0.0663 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AH 93-W-215 (ah93w215-il)