GOE 314 (HANSA-BRANDENBURG) AIRFOIL (goe314-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 314 (HANSA-BRANDENBURG) AIRFOIL (goe314-il) Reynolds number: 200,000 Max Cl/Cd: 70.53 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe314-il-200000.txt Download as CSV file: xf-goe314-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 314 (HANSA-BRANDENBURG) AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.000 -0.3182 0.09545 0.09197 -0.0254 1.0000 0.0398
-7.750 -0.3285 0.09417 0.09077 -0.0275 1.0000 0.0400
-7.500 -0.3291 0.09205 0.08868 -0.0311 1.0000 0.0401
-7.250 -0.3273 0.08838 0.08506 -0.0313 1.0000 0.0403
-7.000 -0.3219 0.08431 0.08105 -0.0262 1.0000 0.0408
-6.750 -0.3194 0.08166 0.07845 -0.0239 1.0000 0.0412
-6.500 -0.3206 0.07952 0.07637 -0.0220 1.0000 0.0418
-6.250 -0.3264 0.07785 0.07476 -0.0201 1.0000 0.0423
-6.000 -0.3324 0.07622 0.07317 -0.0185 0.9997 0.0428
-5.750 -0.2970 0.07173 0.06861 -0.0264 0.9942 0.0444
-5.500 -0.2398 0.06732 0.06394 -0.0423 0.9855 0.0478
-5.250 -0.2014 0.06197 0.05840 -0.0506 0.9777 0.0486
-5.000 -0.1787 0.05766 0.05417 -0.0522 0.9727 0.0494
-4.750 -0.1503 0.05430 0.05078 -0.0551 0.9655 0.0507
-4.500 -0.1141 0.05086 0.04725 -0.0599 0.9591 0.0526
-4.250 -0.0757 0.04766 0.04389 -0.0648 0.9509 0.0556
-4.000 -0.0244 0.04407 0.03982 -0.0718 0.9443 0.0587
-3.750 0.0020 0.04060 0.03642 -0.0737 0.9360 0.0600
-3.500 0.0363 0.03797 0.03375 -0.0766 0.9286 0.0625
-3.250 0.0707 0.03574 0.03134 -0.0787 0.9171 0.0663
-3.000 0.1102 0.03340 0.02854 -0.0812 0.9057 0.0709
-2.750 0.1393 0.03083 0.02598 -0.0826 0.8934 0.0729
-2.500 0.1687 0.02910 0.02413 -0.0834 0.8788 0.0765
-2.250 0.2008 0.02798 0.02252 -0.0834 0.8624 0.0841
-2.000 0.2235 0.02597 0.02054 -0.0832 0.8445 0.0870
-1.750 0.2521 0.02579 0.01989 -0.0823 0.8255 0.0976
-1.500 0.2739 0.02355 0.01768 -0.0818 0.8062 0.1004
-1.250 0.3005 0.02319 0.01693 -0.0808 0.7860 0.1119
-1.000 0.3224 0.02142 0.01516 -0.0801 0.7638 0.1163
-0.750 0.3463 0.02052 0.01404 -0.0791 0.7396 0.1293
-0.500 0.3695 0.01963 0.01298 -0.0781 0.7136 0.1449
-0.250 0.3924 0.01881 0.01201 -0.0772 0.6861 0.1639
0.500 0.4786 0.01681 0.00848 -0.0725 0.6091 0.0830
0.750 0.5037 0.01560 0.00714 -0.0717 0.5871 0.0795
1.000 0.5291 0.01510 0.00645 -0.0708 0.5676 0.0781
1.250 0.5543 0.01488 0.00603 -0.0700 0.5492 0.0799
1.500 0.5794 0.01470 0.00569 -0.0691 0.5321 0.0816
1.750 0.6045 0.01449 0.00537 -0.0683 0.5166 0.0824
2.000 0.6291 0.01413 0.00500 -0.0674 0.5032 0.0846
2.250 0.6537 0.01398 0.00486 -0.0667 0.4916 0.0891
2.500 0.6788 0.01402 0.00481 -0.0660 0.4810 0.0962
2.750 0.7032 0.01386 0.00469 -0.0652 0.4700 0.1040
3.000 0.7281 0.01385 0.00465 -0.0645 0.4597 0.1189
3.250 0.7819 0.01225 0.00471 -0.0701 0.4471 1.0000
3.500 0.8061 0.01248 0.00482 -0.0692 0.4375 1.0000
3.750 0.8302 0.01272 0.00499 -0.0684 0.4278 1.0000
4.000 0.8542 0.01301 0.00514 -0.0675 0.4182 1.0000
4.250 0.8778 0.01319 0.00532 -0.0666 0.4072 1.0000
4.500 0.9015 0.01343 0.00551 -0.0657 0.3970 1.0000
4.750 0.9252 0.01370 0.00568 -0.0649 0.3874 1.0000
5.000 0.9489 0.01390 0.00593 -0.0640 0.3772 1.0000
5.250 0.9723 0.01416 0.00614 -0.0632 0.3670 1.0000
5.500 0.9954 0.01440 0.00632 -0.0622 0.3562 1.0000
5.750 1.0186 0.01461 0.00658 -0.0613 0.3450 1.0000
6.000 1.0417 0.01488 0.00683 -0.0604 0.3347 1.0000
6.250 1.0645 0.01518 0.00707 -0.0595 0.3248 1.0000
6.500 1.0876 0.01542 0.00738 -0.0586 0.3144 1.0000
6.750 1.1103 0.01576 0.00772 -0.0578 0.3052 1.0000
7.000 1.1329 0.01608 0.00804 -0.0568 0.2961 1.0000
7.250 1.1557 0.01642 0.00842 -0.0560 0.2873 1.0000
7.500 1.1779 0.01681 0.00878 -0.0550 0.2797 1.0000
7.750 1.2005 0.01714 0.00923 -0.0542 0.2716 1.0000
8.000 1.2221 0.01755 0.00959 -0.0532 0.2642 1.0000
8.250 1.2443 0.01787 0.01004 -0.0523 0.2564 1.0000
8.750 1.2864 0.01855 0.01085 -0.0502 0.2396 1.0000
9.000 1.3064 0.01891 0.01125 -0.0490 0.2304 1.0000
9.250 1.3255 0.01929 0.01165 -0.0477 0.2204 1.0000
9.500 1.3452 0.01964 0.01210 -0.0465 0.2092 1.0000
9.750 1.3636 0.02006 0.01261 -0.0451 0.1972 1.0000
10.000 1.3807 0.02055 0.01314 -0.0436 0.1828 1.0000
10.250 1.3954 0.02120 0.01377 -0.0418 0.1646 1.0000
10.500 1.4080 0.02200 0.01453 -0.0397 0.1371 1.0000
10.750 1.4074 0.02356 0.01573 -0.0361 0.0894 1.0000
11.000 1.4038 0.02524 0.01730 -0.0320 0.0761 1.0000
11.250 1.4018 0.02685 0.01897 -0.0285 0.0693 1.0000
11.500 1.3950 0.02883 0.02102 -0.0249 0.0636 1.0000
11.750 1.3874 0.03104 0.02338 -0.0219 0.0585 1.0000
12.000 1.3703 0.03420 0.02659 -0.0191 0.0549 1.0000
12.250 1.3636 0.03694 0.02949 -0.0175 0.0505 1.0000
12.500 1.3554 0.04004 0.03268 -0.0165 0.0473 1.0000
12.750 1.3423 0.04384 0.03651 -0.0158 0.0450 1.0000
13.000 1.3373 0.04708 0.03985 -0.0155 0.0428 1.0000
13.250 1.3350 0.05022 0.04312 -0.0156 0.0402 1.0000
13.500 1.3322 0.05344 0.04642 -0.0157 0.0386 1.0000
13.750 1.3288 0.05679 0.04983 -0.0160 0.0372 1.0000
14.000 1.3260 0.05990 0.05290 -0.0155 0.0357 1.0000
14.250 1.3266 0.06298 0.05616 -0.0159 0.0345 1.0000
14.500 1.3274 0.06603 0.05932 -0.0163 0.0333 1.0000
14.750 1.3271 0.06930 0.06270 -0.0169 0.0320 1.0000
15.000 1.3289 0.07225 0.06571 -0.0173 0.0311 1.0000
15.250 1.3282 0.07562 0.06911 -0.0182 0.0301 1.0000
15.500 1.3326 0.07803 0.07151 -0.0176 0.0290 1.0000
15.750 1.3325 0.08154 0.07522 -0.0184 0.0285 1.0000
16.000 1.3335 0.08492 0.07875 -0.0190 0.0280 1.0000
16.250 1.3329 0.08860 0.08260 -0.0198 0.0274 1.0000
16.500 1.3319 0.09240 0.08656 -0.0207 0.0269 1.0000
16.750 1.3291 0.09657 0.09089 -0.0221 0.0265 1.0000
17.000 1.3254 0.10098 0.09547 -0.0236 0.0262 1.0000
17.250 1.3199 0.10576 0.10041 -0.0256 0.0258 1.0000
17.500 1.3131 0.11085 0.10567 -0.0280 0.0256 1.0000
17.750 1.3052 0.11625 0.11122 -0.0307 0.0252 1.0000
18.000 1.2951 0.12223 0.11738 -0.0339 0.0251 1.0000
18.250 1.2871 0.12779 0.12306 -0.0371 0.0248 1.0000
18.500 1.2802 0.13320 0.12858 -0.0403 0.0244 1.0000
18.750 1.2549 0.14320 0.13888 -0.0465 0.0248 1.0000
19.000 1.1960 0.16260 0.15873 -0.0595 0.0264 1.0000
19.250 1.1496 0.18060 0.17693 -0.0714 0.0277 1.0000
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Polar data table (+)
Polar graphs
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