GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 735 AIRFOIL (goe735-il) Reynolds number: 1,000,000 Max Cl/Cd: 105.03 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe735-il-1000000.txt Download as CSV file: xf-goe735-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 735 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 -1.0682 0.08044 0.07711 -0.0500 1.0000 0.0330
-19.250 -1.1202 0.06978 0.06627 -0.0564 1.0000 0.0329
-19.000 -1.1627 0.06025 0.05656 -0.0624 1.0000 0.0330
-18.750 -1.1910 0.05261 0.04875 -0.0675 1.0000 0.0332
-18.500 -1.2100 0.04655 0.04254 -0.0715 1.0000 0.0333
-18.250 -1.2185 0.04224 0.03812 -0.0740 1.0000 0.0336
-18.000 -1.2241 0.03863 0.03440 -0.0758 1.0000 0.0339
-17.750 -1.2260 0.03574 0.03142 -0.0767 1.0000 0.0343
-17.500 -1.2244 0.03342 0.02902 -0.0770 1.0000 0.0346
-17.250 -1.2214 0.03144 0.02696 -0.0769 1.0000 0.0349
-17.000 -1.1959 0.02971 0.02513 -0.0800 0.9468 0.0354
-16.750 -1.1784 0.02758 0.02266 -0.0829 0.8602 0.0362
-16.500 -1.1799 0.02629 0.02121 -0.0806 0.8323 0.0365
-16.250 -1.1780 0.02515 0.01996 -0.0784 0.8153 0.0372
-16.000 -1.1732 0.02420 0.01891 -0.0762 0.8026 0.0377
-15.750 -1.1668 0.02331 0.01793 -0.0741 0.7920 0.0382
-15.500 -1.1573 0.02261 0.01714 -0.0720 0.7830 0.0389
-15.250 -1.1471 0.02192 0.01638 -0.0700 0.7748 0.0394
-15.000 -1.1380 0.02124 0.01560 -0.0677 0.7670 0.0400
-14.750 -1.1307 0.02045 0.01478 -0.0651 0.7605 0.0410
-14.500 -1.1199 0.01982 0.01411 -0.0628 0.7538 0.0418
-14.250 -1.1074 0.01931 0.01352 -0.0606 0.7468 0.0427
-14.000 -1.0929 0.01883 0.01299 -0.0586 0.7414 0.0437
-13.750 -1.0783 0.01836 0.01247 -0.0565 0.7356 0.0446
-13.500 -1.0658 0.01781 0.01189 -0.0541 0.7297 0.0460
-13.250 -1.0507 0.01737 0.01141 -0.0520 0.7235 0.0473
-13.000 -1.0335 0.01699 0.01099 -0.0502 0.7184 0.0487
-12.750 -1.0174 0.01657 0.01054 -0.0482 0.7125 0.0502
-12.500 -1.0006 0.01618 0.01012 -0.0462 0.7066 0.0521
-12.250 -0.9818 0.01587 0.00977 -0.0445 0.7013 0.0540
-12.000 -0.9638 0.01551 0.00940 -0.0426 0.6954 0.0560
-11.750 -0.9451 0.01520 0.00907 -0.0409 0.6890 0.0580
-11.500 -0.9249 0.01499 0.00881 -0.0393 0.6829 0.0600
-11.250 -0.9055 0.01470 0.00852 -0.0376 0.6775 0.0620
-11.000 -0.8849 0.01447 0.00827 -0.0361 0.6707 0.0641
-10.750 -0.8621 0.01431 0.00805 -0.0349 0.6633 0.0661
-10.500 -0.8394 0.01405 0.00778 -0.0338 0.6571 0.0681
-10.250 -0.8163 0.01383 0.00755 -0.0327 0.6496 0.0702
-10.000 -0.7923 0.01367 0.00734 -0.0318 0.6419 0.0720
-9.750 -0.7672 0.01353 0.00716 -0.0310 0.6339 0.0735
-9.500 -0.7446 0.01327 0.00686 -0.0299 0.6249 0.0755
-9.250 -0.7202 0.01308 0.00667 -0.0290 0.6163 0.0773
-9.000 -0.6953 0.01294 0.00648 -0.0282 0.6067 0.0790
-8.750 -0.6696 0.01283 0.00632 -0.0275 0.5976 0.0805
-8.500 -0.6450 0.01266 0.00609 -0.0267 0.5872 0.0822
-8.250 -0.6208 0.01246 0.00587 -0.0258 0.5776 0.0841
-8.000 -0.5955 0.01233 0.00571 -0.0251 0.5673 0.0858
-7.750 -0.5697 0.01222 0.00556 -0.0245 0.5587 0.0874
-7.500 -0.5436 0.01213 0.00541 -0.0239 0.5496 0.0887
-7.250 -0.5182 0.01200 0.00522 -0.0232 0.5412 0.0904
-7.000 -0.4933 0.01180 0.00502 -0.0224 0.5329 0.0926
-6.750 -0.4677 0.01170 0.00488 -0.0218 0.5242 0.0943
-6.500 -0.4412 0.01159 0.00475 -0.0213 0.5181 0.0960
-6.250 -0.4146 0.01152 0.00463 -0.0208 0.5110 0.0975
-6.000 -0.3883 0.01144 0.00450 -0.0202 0.5039 0.0991
-5.750 -0.3628 0.01125 0.00433 -0.0196 0.4982 0.1023
-5.500 -0.3363 0.01116 0.00423 -0.0191 0.4916 0.1046
-5.250 -0.3098 0.01111 0.00412 -0.0186 0.4849 0.1065
-5.000 -0.2825 0.01102 0.00402 -0.0182 0.4802 0.1080
-4.750 -0.2566 0.01088 0.00386 -0.0177 0.4748 0.1106
-4.500 -0.2307 0.01077 0.00374 -0.0171 0.4690 0.1133
-4.250 -0.2039 0.01069 0.00365 -0.0167 0.4641 0.1157
-4.000 -0.1766 0.01062 0.00356 -0.0163 0.4594 0.1181
-3.750 -0.1496 0.01056 0.00347 -0.0159 0.4541 0.1203
-3.500 -0.1239 0.01047 0.00336 -0.0153 0.4483 0.1242
-3.250 -0.0968 0.01038 0.00329 -0.0150 0.4448 0.1277
-3.000 -0.0694 0.01032 0.00323 -0.0147 0.4408 0.1308
-2.750 -0.0428 0.01024 0.00314 -0.0142 0.4364 0.1356
-2.500 -0.0164 0.01019 0.00309 -0.0138 0.4315 0.1406
-2.250 0.0108 0.01017 0.00305 -0.0135 0.4271 0.1447
-2.000 0.0376 0.01006 0.00298 -0.0131 0.4237 0.1522
-1.750 0.0646 0.01001 0.00293 -0.0128 0.4196 0.1589
-1.500 0.0908 0.00994 0.00289 -0.0123 0.4156 0.1694
-1.250 0.1168 0.00991 0.00287 -0.0118 0.4108 0.1813
-1.000 0.1432 0.00980 0.00284 -0.0114 0.4081 0.1982
-0.750 0.1691 0.00967 0.00281 -0.0109 0.4051 0.2237
-0.500 0.1942 0.00952 0.00278 -0.0103 0.4015 0.2589
-0.250 0.2188 0.00940 0.00278 -0.0096 0.3976 0.2994
0.000 0.2430 0.00931 0.00279 -0.0089 0.3930 0.3390
0.250 0.2678 0.00918 0.00280 -0.0082 0.3903 0.3806
0.500 0.2917 0.00898 0.00278 -0.0073 0.3878 0.4339
0.750 0.3110 0.00864 0.00278 -0.0057 0.3849 0.5312
1.000 0.3294 0.00836 0.00278 -0.0037 0.3819 0.6216
1.250 0.3450 0.00810 0.00281 -0.0011 0.3787 0.7117
1.500 0.3615 0.00795 0.00290 0.0014 0.3749 0.7906
1.750 0.3855 0.00787 0.00299 0.0025 0.3725 0.8417
2.000 0.4152 0.00786 0.00309 0.0023 0.3700 0.8776
2.250 0.4490 0.00794 0.00321 0.0013 0.3668 0.8996
2.500 0.4830 0.00806 0.00333 0.0001 0.3634 0.9160
2.750 0.5162 0.00824 0.00348 -0.0010 0.3598 0.9283
3.000 0.5549 0.00846 0.00367 -0.0032 0.3560 0.9363
3.250 0.5839 0.00858 0.00380 -0.0033 0.3542 0.9457
3.500 0.6243 0.00876 0.00397 -0.0058 0.3517 0.9507
3.750 0.6695 0.00902 0.00421 -0.0092 0.3485 0.9545
4.000 0.7066 0.00930 0.00444 -0.0111 0.3452 0.9591
4.250 0.7349 0.00956 0.00466 -0.0112 0.3416 0.9645
4.500 0.7745 0.00979 0.00486 -0.0137 0.3385 0.9656
4.750 0.8140 0.00994 0.00501 -0.0161 0.3367 0.9668
5.000 0.8542 0.01011 0.00518 -0.0186 0.3343 0.9685
5.250 0.8930 0.01031 0.00536 -0.0210 0.3315 0.9707
5.500 0.9266 0.01051 0.00553 -0.0223 0.3285 0.9736
5.750 0.9490 0.01077 0.00576 -0.0214 0.3256 0.9785
6.000 0.9853 0.01099 0.00595 -0.0234 0.3222 0.9795
6.250 1.0227 0.01109 0.00606 -0.0256 0.3204 0.9804
6.500 1.0586 0.01120 0.00618 -0.0274 0.3181 0.9816
6.750 1.0929 0.01134 0.00632 -0.0290 0.3153 0.9829
7.000 1.1255 0.01151 0.00647 -0.0303 0.3126 0.9845
7.250 1.1564 0.01174 0.00667 -0.0313 0.3095 0.9866
7.500 1.1841 0.01205 0.00695 -0.0318 0.3061 0.9891
7.750 1.2102 0.01222 0.00715 -0.0318 0.3048 0.9917
8.000 1.2443 0.01231 0.00726 -0.0334 0.3029 0.9925
8.250 1.2780 0.01243 0.00740 -0.0350 0.3007 0.9936
8.500 1.3106 0.01259 0.00757 -0.0365 0.2983 0.9950
8.750 1.3419 0.01280 0.00777 -0.0377 0.2959 0.9966
9.000 1.3717 0.01306 0.00802 -0.0388 0.2931 0.9983
9.250 1.4005 0.01341 0.00834 -0.0398 0.2899 0.9997
9.500 1.4202 0.01356 0.00855 -0.0387 0.2886 1.0000
9.750 1.4322 0.01376 0.00878 -0.0362 0.2870 1.0000
10.000 1.4354 0.01398 0.00903 -0.0321 0.2855 1.0000
10.250 1.4294 0.01426 0.00935 -0.0266 0.2839 1.0000
10.500 1.4283 0.01469 0.00981 -0.0224 0.2821 1.0000
10.750 1.4306 0.01523 0.01037 -0.0189 0.2802 1.0000
11.000 1.4340 0.01588 0.01102 -0.0159 0.2780 1.0000
11.250 1.4370 0.01666 0.01181 -0.0131 0.2753 1.0000
11.500 1.4465 0.01728 0.01245 -0.0112 0.2736 1.0000
11.750 1.4592 0.01781 0.01304 -0.0097 0.2722 1.0000
12.000 1.4713 0.01841 0.01368 -0.0083 0.2705 1.0000
12.250 1.4830 0.01907 0.01437 -0.0069 0.2684 1.0000
12.500 1.4931 0.01986 0.01518 -0.0055 0.2658 1.0000
12.750 1.5012 0.02080 0.01614 -0.0040 0.2635 1.0000
13.000 1.5047 0.02205 0.01737 -0.0023 0.2597 1.0000
13.250 1.5172 0.02284 0.01821 -0.0013 0.2575 1.0000
13.500 1.5297 0.02365 0.01907 -0.0005 0.2552 1.0000
13.750 1.5398 0.02463 0.02008 0.0005 0.2523 1.0000
14.000 1.5453 0.02596 0.02142 0.0016 0.2488 1.0000
14.250 1.5482 0.02748 0.02295 0.0028 0.2457 1.0000
14.500 1.5562 0.02872 0.02423 0.0036 0.2423 1.0000
14.750 1.5662 0.02984 0.02540 0.0042 0.2400 1.0000
15.000 1.5715 0.03138 0.02697 0.0049 0.2359 1.0000
15.250 1.5704 0.03351 0.02910 0.0057 0.2318 1.0000
15.500 1.5735 0.03534 0.03096 0.0063 0.2286 1.0000
15.750 1.5819 0.03679 0.03247 0.0066 0.2255 1.0000
16.000 1.5855 0.03869 0.03441 0.0070 0.2224 1.0000
16.250 1.5800 0.04143 0.03716 0.0074 0.2177 1.0000
16.500 1.5802 0.04373 0.03949 0.0077 0.2138 1.0000
16.750 1.5826 0.04587 0.04169 0.0079 0.2105 1.0000
17.000 1.5790 0.04860 0.04445 0.0080 0.2064 1.0000
17.250 1.5685 0.05203 0.04789 0.0082 0.2021 1.0000
17.500 1.5693 0.05443 0.05035 0.0081 0.1995 1.0000
17.750 1.5664 0.05723 0.05319 0.0080 0.1954 1.0000
18.000 1.5572 0.06069 0.05667 0.0079 0.1914 1.0000
18.250 1.5453 0.06452 0.06054 0.0077 0.1876 1.0000
18.500 1.5433 0.06734 0.06341 0.0074 0.1838 1.0000
18.750 1.5374 0.07060 0.06671 0.0070 0.1807 1.0000
19.000 1.5192 0.07530 0.07142 0.0064 0.1761 1.0000
19.250 1.5187 0.07804 0.07422 0.0060 0.1736 1.0000
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