Griffith 30% Suction Airfoil (griffith30symsuction-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: Griffith 30% Suction Airfoil (griffith30symsuction-il) Reynolds number: 1,000,000 Max Cl/Cd: 17.27 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-griffith30symsuction-il-1000000.txt Download as CSV file: xf-griffith30symsuction-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: Griffith 30% Suction 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
------ -------- --------- --------- -------- -------- --------
-19.500 -0.9362 0.08219 0.07681 -0.0910 0.7884 0.0348
-19.250 -0.9350 0.08007 0.07469 -0.0908 0.7882 0.0402
-19.000 -0.9342 0.07796 0.07260 -0.0906 0.7880 0.0469
-18.750 -0.9307 0.07618 0.07085 -0.0903 0.7879 0.0544
-18.500 -0.9261 0.07452 0.06921 -0.0900 0.7877 0.0612
-18.250 -0.9210 0.07295 0.06765 -0.0897 0.7875 0.0674
-18.000 -0.9134 0.07165 0.06637 -0.0894 0.7874 0.0731
-17.750 -0.9039 0.07052 0.06523 -0.0892 0.7872 0.0782
-17.500 -0.8980 0.06915 0.06387 -0.0886 0.7871 0.0838
-17.250 -0.8909 0.06798 0.06270 -0.0878 0.7869 0.0892
-17.000 -0.8832 0.06695 0.06168 -0.0869 0.7867 0.0957
-16.750 -0.8764 0.06585 0.06062 -0.0859 0.7866 0.1035
-16.500 -0.8704 0.06471 0.05952 -0.0849 0.7865 0.1125
-16.250 -0.8651 0.06358 0.05843 -0.0838 0.7864 0.1233
-16.000 -0.8575 0.06268 0.05759 -0.0827 0.7863 0.1353
-15.750 -0.8494 0.06187 0.05683 -0.0816 0.7862 0.1469
-15.500 -0.8418 0.06109 0.05610 -0.0803 0.7861 0.1568
-15.250 -0.8317 0.06053 0.05554 -0.0791 0.7860 0.1640
-15.000 -0.8234 0.05996 0.05500 -0.0777 0.7859 0.1721
-14.750 -0.7825 0.05914 0.05423 -0.0868 0.7830 0.1804
-14.500 -0.7692 0.05846 0.05357 -0.0864 0.7818 0.1867
-14.250 -0.7566 0.05778 0.05291 -0.0856 0.7810 0.1930
-14.000 -0.7420 0.05721 0.05232 -0.0849 0.7803 0.1982
-13.750 -0.7281 0.05660 0.05169 -0.0841 0.7798 0.2030
-13.500 -0.7162 0.05595 0.05106 -0.0830 0.7794 0.2093
-13.250 -0.7022 0.05546 0.05058 -0.0820 0.7791 0.2144
-13.000 -0.6861 0.05510 0.05019 -0.0813 0.7788 0.2190
-12.750 -0.6697 0.05451 0.04960 -0.0819 0.7737 0.2240
-12.500 -0.6588 0.05359 0.04871 -0.0806 0.7725 0.2319
-12.250 -0.6447 0.05288 0.04800 -0.0797 0.7718 0.2374
-12.000 -0.6273 0.05240 0.04750 -0.0791 0.7712 0.2411
-11.750 -0.6096 0.05195 0.04701 -0.0785 0.7708 0.2441
-11.500 -0.5965 0.05126 0.04634 -0.0773 0.7704 0.2512
-11.250 -0.5828 0.05062 0.04572 -0.0761 0.7701 0.2572
-11.000 -0.5735 0.05027 0.04538 -0.0753 0.7650 0.2628
-10.750 -0.5616 0.04964 0.04476 -0.0741 0.7638 0.2716
-10.500 -0.5513 0.04886 0.04404 -0.0725 0.7629 0.2842
-10.250 -0.5427 0.04799 0.04325 -0.0706 0.7623 0.3014
-10.000 -0.5406 0.04683 0.04222 -0.0678 0.7618 0.3274
-9.750 -0.5410 0.04556 0.04109 -0.0646 0.7613 0.3613
-9.500 -0.5382 0.04446 0.04011 -0.0617 0.7609 0.3894
-9.250 -0.5343 0.04341 0.03915 -0.0589 0.7606 0.4119
-9.000 -0.5547 0.04316 0.03897 -0.0525 0.7544 0.4282
-8.750 -0.5554 0.04222 0.03813 -0.0488 0.7531 0.4496
-8.500 -0.5657 0.04078 0.03682 -0.0435 0.7522 0.4787
-8.250 -0.5937 0.03867 0.03501 -0.0352 0.7514 0.5338
-8.000 -0.6028 0.03729 0.03382 -0.0297 0.7509 0.5782
-7.750 -0.5921 0.03661 0.03318 -0.0276 0.7505 0.5977
-7.500 -0.6319 0.03682 0.03345 -0.0157 0.7432 0.6076
-7.250 -0.6253 0.03623 0.03284 -0.0127 0.7421 0.6181
-7.000 -0.5996 0.03631 0.03296 -0.0130 0.7415 0.6263
-6.750 -0.5961 0.03542 0.03203 -0.0096 0.7408 0.6351
-6.500 -0.5638 0.03568 0.03231 -0.0110 0.7404 0.6401
-6.250 -0.5332 0.03584 0.03248 -0.0121 0.7401 0.6456
-6.000 -0.5395 0.03452 0.03112 -0.0070 0.7396 0.6545
-5.750 -0.4951 0.03517 0.03178 -0.0105 0.7394 0.6573
-5.500 -0.5063 0.03619 0.03285 -0.0039 0.7322 0.6606
-5.250 -0.4860 0.03613 0.03278 -0.0033 0.7311 0.6653
-5.000 -0.4848 0.03524 0.03187 0.0007 0.7301 0.6724
-4.750 -0.4456 0.03574 0.03237 -0.0020 0.7297 0.6739
-4.500 -0.4095 0.03610 0.03273 -0.0041 0.7293 0.6753
-4.250 -0.3770 0.03631 0.03293 -0.0056 0.7290 0.6769
-4.000 -0.3483 0.03637 0.03299 -0.0064 0.7286 0.6791
-3.750 -0.3451 0.03541 0.03199 -0.0028 0.7280 0.6859
-3.500 -0.3181 0.03534 0.03192 -0.0033 0.7277 0.6880
-3.250 -0.2841 0.03553 0.03210 -0.0051 0.7275 0.6887
-3.000 -0.2505 0.03571 0.03227 -0.0068 0.7273 0.6894
-2.750 -0.2179 0.03587 0.03242 -0.0083 0.7270 0.6901
-2.500 -0.1857 0.03602 0.03257 -0.0097 0.7268 0.6907
-2.000 -0.2114 0.03597 0.03253 0.0033 0.7166 0.7010
-1.750 -0.1831 0.03602 0.03257 0.0025 0.7162 0.7020
-1.500 -0.1522 0.03615 0.03269 0.0013 0.7159 0.7023
-1.250 -0.1212 0.03627 0.03280 0.0001 0.7156 0.7027
-1.000 -0.0892 0.03642 0.03295 -0.0013 0.7153 0.7030
-0.750 -0.0566 0.03651 0.03304 -0.0028 0.7151 0.7034
-0.500 -0.0234 0.03655 0.03308 -0.0044 0.7149 0.7037
-0.250 0.0124 0.03658 0.03310 -0.0064 0.7147 0.7041
0.000 0.0495 0.03654 0.03306 -0.0086 0.7145 0.7044
0.250 0.0352 0.03796 0.03451 -0.0019 0.7045 0.7054
0.500 0.0676 0.03787 0.03442 -0.0033 0.7041 0.7060
0.750 0.0984 0.03777 0.03432 -0.0045 0.7037 0.7068
1.000 0.1279 0.03758 0.03413 -0.0054 0.7033 0.7078
1.250 0.1213 0.03626 0.03280 -0.0001 0.7026 0.7156
1.500 0.1522 0.03614 0.03268 -0.0013 0.7023 0.7159
1.750 0.1831 0.03602 0.03256 -0.0025 0.7020 0.7162
2.000 0.2114 0.03597 0.03252 -0.0033 0.7010 0.7166
2.250 0.2035 0.03727 0.03384 0.0023 0.6921 0.7174
2.500 0.2337 0.03710 0.03368 0.0012 0.6914 0.7179
2.750 0.2638 0.03691 0.03349 0.0001 0.6906 0.7185
3.000 0.2934 0.03669 0.03328 -0.0009 0.6898 0.7193
3.250 0.3226 0.03646 0.03306 -0.0018 0.6890 0.7202
3.500 0.3505 0.03612 0.03272 -0.0025 0.6883 0.7216
3.750 0.3538 0.03507 0.03165 0.0013 0.6873 0.7280
4.000 0.3484 0.03637 0.03298 0.0064 0.6791 0.7286
4.250 0.3771 0.03631 0.03293 0.0055 0.6769 0.7290
4.500 0.4094 0.03611 0.03274 0.0041 0.6754 0.7293
4.750 0.4455 0.03574 0.03237 0.0020 0.6739 0.7297
5.000 0.4846 0.03524 0.03187 -0.0006 0.6724 0.7301
5.250 0.4863 0.03611 0.03277 0.0032 0.6654 0.7311
5.500 0.5063 0.03617 0.03283 0.0039 0.6607 0.7323
5.750 0.4953 0.03515 0.03177 0.0105 0.6573 0.7395
6.000 0.5396 0.03451 0.03111 0.0070 0.6545 0.7396
6.250 0.5333 0.03582 0.03247 0.0121 0.6456 0.7401
6.500 0.5639 0.03566 0.03229 0.0110 0.6401 0.7405
6.750 0.5965 0.03539 0.03201 0.0095 0.6351 0.7408
7.000 0.5997 0.03629 0.03294 0.0130 0.6264 0.7415
7.250 0.6252 0.03621 0.03283 0.0128 0.6181 0.7421
7.500 0.6317 0.03680 0.03343 0.0158 0.6077 0.7433
7.750 0.5924 0.03659 0.03316 0.0275 0.5978 0.7505
8.000 0.6033 0.03727 0.03379 0.0297 0.5782 0.7509
8.250 0.5947 0.03863 0.03496 0.0350 0.5343 0.7514
8.500 0.5666 0.04073 0.03678 0.0434 0.4791 0.7522
8.750 0.5563 0.04217 0.03808 0.0487 0.4501 0.7532
9.000 0.5551 0.04311 0.03893 0.0525 0.4284 0.7544
9.250 0.5353 0.04337 0.03910 0.0587 0.4120 0.7606
9.500 0.5389 0.04443 0.04008 0.0615 0.3892 0.7610
9.750 0.5420 0.04552 0.04106 0.0644 0.3615 0.7613
10.000 0.5416 0.04679 0.04217 0.0677 0.3273 0.7618
10.250 0.5436 0.04795 0.04321 0.0705 0.3011 0.7623
10.500 0.5522 0.04882 0.04399 0.0724 0.2840 0.7630
10.750 0.5624 0.04960 0.04472 0.0739 0.2713 0.7638
11.000 0.5747 0.05021 0.04531 0.0751 0.2628 0.7651
11.250 0.5842 0.05057 0.04566 0.0758 0.2571 0.7702
11.500 0.5979 0.05121 0.04629 0.0770 0.2511 0.7705
11.750 0.6109 0.05190 0.04696 0.0783 0.2440 0.7708
12.000 0.6288 0.05234 0.04744 0.0788 0.2410 0.7713
12.250 0.6462 0.05282 0.04794 0.0794 0.2372 0.7718
12.500 0.6603 0.05354 0.04865 0.0804 0.2315 0.7726
12.750 0.6714 0.05445 0.04953 0.0816 0.2239 0.7738
13.000 0.6880 0.05503 0.05012 0.0810 0.2189 0.7788
13.250 0.7040 0.05540 0.05051 0.0817 0.2144 0.7791
13.500 0.7179 0.05589 0.05099 0.0827 0.2091 0.7794
13.750 0.7298 0.05656 0.05164 0.0838 0.2025 0.7799
14.000 0.7443 0.05713 0.05224 0.0846 0.1980 0.7804
14.250 0.7587 0.05771 0.05284 0.0853 0.1928 0.7810
14.500 0.7711 0.05841 0.05351 0.0860 0.1863 0.7819
14.750 0.7851 0.05908 0.05417 0.0863 0.1802 0.7833
15.000 0.8256 0.05989 0.05492 0.0773 0.1717 0.7859
15.250 0.8344 0.06044 0.05544 0.0787 0.1637 0.7860
15.500 0.8444 0.06101 0.05601 0.0798 0.1562 0.7861
15.750 0.8521 0.06180 0.05675 0.0811 0.1464 0.7862
16.000 0.8600 0.06263 0.05752 0.0822 0.1347 0.7863
16.250 0.8674 0.06354 0.05838 0.0833 0.1225 0.7864
16.500 0.8732 0.06466 0.05945 0.0845 0.1117 0.7865
16.750 0.8792 0.06580 0.06055 0.0854 0.1029 0.7866
17.000 0.8862 0.06688 0.06161 0.0864 0.0952 0.7867
17.250 0.8939 0.06793 0.06264 0.0873 0.0888 0.7869
17.500 0.9016 0.06906 0.06377 0.0880 0.0833 0.7871
17.750 0.9073 0.07046 0.06516 0.0886 0.0778 0.7873
18.000 0.9169 0.07159 0.06630 0.0888 0.0726 0.7874
18.250 0.9247 0.07288 0.06757 0.0891 0.0669 0.7876
18.500 0.9296 0.07448 0.06915 0.0894 0.0606 0.7877
18.750 0.9340 0.07616 0.07082 0.0897 0.0538 0.7879
19.000 0.9381 0.07792 0.07254 0.0899 0.0463 0.7881
19.250 0.9390 0.08002 0.07463 0.0902 0.0396 0.7883
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