EH 3.0/12 (eh3012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: EH 3.0/12 (eh3012-il) Reynolds number: 1,000,000 Max Cl/Cd: 74.08 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-eh3012-il-1000000-n5.txt Download as CSV file: xf-eh3012-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: EH 3.0/12
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 -1.1260 0.04185 0.03879 -0.0443 1.0000 0.0021
-14.500 -1.1485 0.03788 0.03460 -0.0419 1.0000 0.0021
-14.250 -1.1630 0.03500 0.03152 -0.0386 1.0000 0.0021
-14.000 -1.1696 0.03295 0.02931 -0.0350 1.0000 0.0021
-13.750 -1.1699 0.03123 0.02745 -0.0319 1.0000 0.0021
-13.500 -1.1641 0.02955 0.02562 -0.0297 1.0000 0.0021
-13.250 -1.1550 0.02807 0.02400 -0.0277 1.0000 0.0021
-13.000 -1.1433 0.02673 0.02253 -0.0259 1.0000 0.0021
-12.750 -1.1296 0.02553 0.02120 -0.0242 1.0000 0.0021
-12.500 -1.1144 0.02440 0.01996 -0.0227 1.0000 0.0021
-12.250 -1.0978 0.02338 0.01883 -0.0213 1.0000 0.0021
-12.000 -1.0801 0.02244 0.01779 -0.0200 1.0000 0.0020
-11.750 -1.0614 0.02155 0.01681 -0.0188 1.0000 0.0020
-11.500 -1.0419 0.02074 0.01591 -0.0177 1.0000 0.0020
-11.250 -1.0218 0.01997 0.01506 -0.0166 1.0000 0.0020
-11.000 -1.0010 0.01925 0.01426 -0.0156 1.0000 0.0020
-10.500 -0.9428 0.01794 0.01263 -0.0168 0.8843 0.0020
-10.250 -0.9234 0.01753 0.01199 -0.0152 0.8352 0.0019
-10.000 -0.9019 0.01708 0.01136 -0.0141 0.7994 0.0019
-9.750 -0.8794 0.01666 0.01078 -0.0132 0.7673 0.0019
-9.500 -0.8563 0.01624 0.01023 -0.0124 0.7492 0.0019
-9.250 -0.8323 0.01581 0.00970 -0.0117 0.7296 0.0019
-9.000 -0.8083 0.01542 0.00920 -0.0110 0.7143 0.0019
-8.750 -0.7838 0.01503 0.00873 -0.0104 0.6986 0.0018
-8.500 -0.7590 0.01467 0.00828 -0.0099 0.6838 0.0018
-8.250 -0.7341 0.01432 0.00784 -0.0093 0.6693 0.0018
-8.000 -0.7087 0.01403 0.00750 -0.0088 0.6555 0.0017
-7.500 -0.6582 0.01339 0.00666 -0.0079 0.6266 0.0002
-7.250 -0.6327 0.01308 0.00624 -0.0074 0.6121 0.0002
-7.000 -0.6070 0.01281 0.00591 -0.0069 0.6006 0.0002
-6.750 -0.5810 0.01255 0.00559 -0.0065 0.5903 0.0003
-6.500 -0.5549 0.01229 0.00528 -0.0062 0.5813 0.0003
-6.000 -0.5025 0.01183 0.00471 -0.0054 0.5642 0.0004
-5.500 -0.4497 0.01141 0.00419 -0.0047 0.5469 0.0004
-5.250 -0.4233 0.01122 0.00395 -0.0044 0.5377 0.0004
-5.000 -0.3967 0.01104 0.00373 -0.0041 0.5289 0.0005
-4.750 -0.3700 0.01087 0.00351 -0.0038 0.5211 0.0005
-4.500 -0.3413 0.01109 0.00379 -0.0040 0.5128 0.0008
-4.250 -0.3168 0.01050 0.00305 -0.0032 0.5052 0.0008
-4.000 -0.2900 0.01036 0.00288 -0.0029 0.4969 0.0008
-3.750 -0.2628 0.01026 0.00279 -0.0027 0.4902 0.0009
-3.500 -0.2360 0.01011 0.00262 -0.0024 0.4834 0.0020
-2.750 -0.1548 0.00979 0.00222 -0.0017 0.4623 0.0030
-2.500 -0.1283 0.00959 0.00205 -0.0014 0.4565 0.0100
-2.250 -0.1011 0.00950 0.00195 -0.0012 0.4493 0.0114
-2.000 -0.0739 0.00943 0.00185 -0.0010 0.4429 0.0122
-1.750 -0.0465 0.00935 0.00177 -0.0008 0.4369 0.0135
-1.500 -0.0193 0.00928 0.00169 -0.0007 0.4307 0.0168
-1.250 0.0079 0.00919 0.00161 -0.0005 0.4251 0.0229
-1.000 0.0344 0.00904 0.00153 -0.0002 0.4185 0.0420
-0.750 0.0616 0.00897 0.00148 0.0000 0.4129 0.0532
-0.500 0.0891 0.00892 0.00144 0.0001 0.4075 0.0594
-0.250 0.1167 0.00891 0.00141 0.0002 0.4013 0.0609
0.000 0.1440 0.00886 0.00138 0.0003 0.3960 0.0707
0.250 0.1684 0.00848 0.00137 0.0009 0.3911 0.1776
0.500 0.1760 0.00675 0.00119 0.0042 0.3865 0.6663
0.750 0.1984 0.00650 0.00121 0.0055 0.3814 0.7562
1.000 0.2237 0.00652 0.00124 0.0061 0.3627 0.7929
1.250 0.2497 0.00655 0.00128 0.0065 0.3497 0.8177
1.500 0.2758 0.00656 0.00132 0.0070 0.3418 0.8438
1.750 0.3020 0.00662 0.00138 0.0074 0.3284 0.8640
2.000 0.3273 0.00685 0.00147 0.0079 0.2943 0.8804
2.250 0.3535 0.00702 0.00156 0.0082 0.2734 0.8934
2.500 0.3789 0.00729 0.00169 0.0087 0.2423 0.9060
2.750 0.4050 0.00751 0.00183 0.0090 0.2206 0.9177
3.000 0.4318 0.00774 0.00197 0.0091 0.2008 0.9273
3.250 0.4470 0.00928 0.00282 0.0107 0.0206 0.9368
3.500 0.4759 0.00945 0.00297 0.0104 0.0089 0.9417
3.750 0.5043 0.00962 0.00311 0.0102 0.0052 0.9473
4.000 0.5322 0.00977 0.00324 0.0101 0.0056 0.9527
4.250 0.5631 0.00996 0.00342 0.0093 0.0038 0.9565
4.500 0.5934 0.01013 0.00356 0.0086 0.0034 0.9606
4.750 0.6223 0.01031 0.00372 0.0082 0.0033 0.9652
5.000 0.6529 0.01050 0.00390 0.0074 0.0033 0.9683
5.250 0.6851 0.01071 0.00408 0.0062 0.0032 0.9706
5.500 0.7167 0.01098 0.00428 0.0052 0.0026 0.9731
6.000 0.7771 0.01140 0.00475 0.0036 0.0020 0.9792
6.250 0.8070 0.01164 0.00501 0.0029 0.0016 0.9815
6.500 0.8384 0.01189 0.00523 0.0018 0.0020 0.9831
6.750 0.8692 0.01216 0.00549 0.0008 0.0020 0.9851
7.000 0.8993 0.01243 0.00576 -0.0001 0.0020 0.9875
7.250 0.9283 0.01273 0.00608 -0.0007 0.0018 0.9901
7.500 0.9562 0.01305 0.00640 -0.0012 0.0016 0.9927
7.750 0.9865 0.01337 0.00673 -0.0022 0.0016 0.9946
8.000 1.0164 0.01372 0.00711 -0.0031 0.0015 0.9965
8.250 1.0457 0.01412 0.00754 -0.0040 0.0013 0.9983
8.500 1.0746 0.01458 0.00804 -0.0049 0.0011 0.9997
8.750 1.0951 0.01496 0.00844 -0.0040 0.0011 1.0000
9.000 1.1119 0.01537 0.00889 -0.0023 0.0011 1.0000
9.250 1.1307 0.01567 0.00917 -0.0010 0.0013 1.0000
9.500 1.1475 0.01611 0.00964 0.0006 0.0014 1.0000
9.750 1.1631 0.01661 0.01018 0.0023 0.0013 1.0000
10.000 1.1757 0.01728 0.01093 0.0044 0.0012 1.0000
10.250 1.1926 0.01767 0.01132 0.0058 0.0013 1.0000
10.500 1.2075 0.01815 0.01182 0.0075 0.0014 1.0000
10.750 1.2193 0.01875 0.01245 0.0096 0.0014 1.0000
11.000 1.2257 0.01933 0.01307 0.0126 0.0015 1.0000
11.250 1.2291 0.02016 0.01397 0.0156 0.0015 1.0000
11.500 1.2356 0.02109 0.01495 0.0176 0.0015 1.0000
11.750 1.2409 0.02233 0.01626 0.0190 0.0015 1.0000
12.000 1.2496 0.02355 0.01753 0.0198 0.0016 1.0000
12.250 1.2543 0.02533 0.01938 0.0202 0.0017 1.0000
12.500 1.2625 0.02694 0.02104 0.0203 0.0017 1.0000
12.750 1.2633 0.02943 0.02364 0.0202 0.0017 1.0000
13.000 1.2688 0.03154 0.02580 0.0198 0.0017 1.0000
13.250 1.2666 0.03454 0.02890 0.0193 0.0018 1.0000
13.500 1.2717 0.03678 0.03121 0.0189 0.0017 1.0000
13.750 1.2690 0.03991 0.03443 0.0183 0.0017 1.0000
14.000 1.2597 0.04385 0.03847 0.0175 0.0019 1.0000
14.250 1.2641 0.04619 0.04087 0.0170 0.0017 1.0000
14.500 1.2571 0.04991 0.04467 0.0161 0.0018 1.0000
14.750 1.2398 0.05490 0.04978 0.0149 0.0019 1.0000
15.000 1.2385 0.05809 0.05304 0.0141 0.0018 1.0000
15.250 1.2248 0.06297 0.05803 0.0127 0.0020 1.0000
15.500 1.2303 0.06540 0.06049 0.0120 0.0018 1.0000
15.750 1.2124 0.07106 0.06628 0.0102 0.0019 1.0000
16.000 1.2117 0.07440 0.06967 0.0092 0.0019 1.0000
16.250 1.2019 0.07908 0.07443 0.0077 0.0019 1.0000
16.500 1.2009 0.08257 0.07798 0.0065 0.0018 1.0000
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