GOE 336 (MVA H.44) AIRFOIL (goe336-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 336 (MVA H.44) AIRFOIL (goe336-il) Reynolds number: 1,000,000 Max Cl/Cd: 94.86 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe336-il-1000000-n5.txt Download as CSV file: xf-goe336-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 336 (MVA H.44) 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.3448 0.09702 0.09465 -0.0266 0.7583 0.0082
-9.250 -0.3416 0.09337 0.09093 -0.0285 0.7412 0.0086
-9.000 -0.3512 0.08669 0.08422 -0.0323 0.7312 0.0097
-8.750 -0.3433 0.08416 0.08165 -0.0341 0.7203 0.0099
-8.500 -0.3360 0.08150 0.07897 -0.0363 0.7117 0.0101
-8.000 -0.3170 0.07546 0.07287 -0.0423 0.6969 0.0106
-7.750 -0.3054 0.07162 0.06899 -0.0463 0.6898 0.0111
-7.500 -0.3008 0.06224 0.05952 -0.0554 0.6854 0.0128
-7.250 -0.2815 0.06005 0.05728 -0.0576 0.6777 0.0130
-7.000 -0.2617 0.05777 0.05492 -0.0597 0.6703 0.0133
-6.500 -0.2218 0.05078 0.04775 -0.0655 0.6557 0.0146
-6.000 -0.2083 0.02034 0.01596 -0.0739 0.6495 0.0202
-5.500 -0.1606 0.01733 0.01239 -0.0731 0.6330 0.0208
-5.250 -0.1345 0.01679 0.01169 -0.0728 0.6237 0.0210
-5.000 -0.1109 0.01528 0.00987 -0.0723 0.6135 0.0213
-4.750 -0.0866 0.01396 0.00828 -0.0718 0.6031 0.0217
-4.500 -0.0607 0.01325 0.00740 -0.0715 0.5913 0.0219
-4.250 -0.0344 0.01273 0.00674 -0.0712 0.5787 0.0222
-4.000 -0.0077 0.01230 0.00618 -0.0709 0.5660 0.0224
-3.750 0.0192 0.01196 0.00573 -0.0707 0.5539 0.0227
-3.500 0.0464 0.01169 0.00537 -0.0705 0.5436 0.0230
-3.250 0.0734 0.01139 0.00497 -0.0703 0.5341 0.0233
-3.000 0.1007 0.01107 0.00455 -0.0701 0.5255 0.0237
-2.750 0.1279 0.01079 0.00417 -0.0699 0.5177 0.0240
-2.500 0.1554 0.01053 0.00384 -0.0697 0.5103 0.0244
-2.250 0.1827 0.01032 0.00355 -0.0696 0.5035 0.0248
-2.000 0.2102 0.01010 0.00328 -0.0694 0.4974 0.0251
-1.750 0.2376 0.00992 0.00303 -0.0692 0.4913 0.0254
-1.500 0.2650 0.00975 0.00282 -0.0691 0.4861 0.0257
-1.250 0.2925 0.00959 0.00262 -0.0689 0.4807 0.0260
-1.000 0.3198 0.00947 0.00244 -0.0688 0.4743 0.0262
-0.750 0.3472 0.00935 0.00229 -0.0686 0.4671 0.0264
-0.250 0.4018 0.00920 0.00204 -0.0683 0.4511 0.0268
0.000 0.4293 0.00913 0.00195 -0.0681 0.4464 0.0270
0.250 0.4568 0.00910 0.00189 -0.0680 0.4425 0.0273
0.500 0.4844 0.00905 0.00183 -0.0679 0.4377 0.0275
0.750 0.5114 0.00900 0.00174 -0.0677 0.4288 0.0279
1.000 0.5388 0.00896 0.00166 -0.0676 0.4226 0.0288
1.250 0.5662 0.00893 0.00161 -0.0674 0.4165 0.0303
1.500 0.5934 0.00895 0.00160 -0.0673 0.4111 0.0317
1.750 0.6211 0.00894 0.00160 -0.0673 0.4069 0.0333
2.000 0.6486 0.00895 0.00161 -0.0672 0.4018 0.0352
2.500 0.7030 0.00895 0.00170 -0.0670 0.3902 0.0753
2.750 0.7299 0.00903 0.00177 -0.0669 0.3805 0.0872
3.000 0.7570 0.00909 0.00183 -0.0668 0.3696 0.0971
3.250 0.7835 0.00921 0.00192 -0.0666 0.3531 0.1086
3.500 0.8088 0.00944 0.00205 -0.0663 0.3223 0.1233
3.750 0.8277 0.01033 0.00254 -0.0650 0.2285 0.1538
4.000 0.8522 0.01050 0.00279 -0.0646 0.2085 0.2424
4.500 0.9562 0.01008 0.00367 -0.0768 0.1436 0.9993
4.750 0.9831 0.01060 0.00400 -0.0770 0.1120 1.0000
5.000 1.0056 0.01091 0.00424 -0.0761 0.0985 1.0000
5.250 1.0250 0.01151 0.00464 -0.0747 0.0636 1.0000
5.500 1.0475 0.01180 0.00489 -0.0738 0.0550 1.0000
5.750 1.0704 0.01204 0.00511 -0.0730 0.0522 1.0000
6.000 1.0927 0.01232 0.00538 -0.0720 0.0488 1.0000
6.250 1.1149 0.01259 0.00564 -0.0711 0.0455 1.0000
6.500 1.1375 0.01282 0.00588 -0.0702 0.0435 1.0000
6.750 1.1589 0.01314 0.00617 -0.0691 0.0383 1.0000
7.000 1.1756 0.01379 0.00669 -0.0673 0.0156 1.0000
7.250 1.1960 0.01415 0.00706 -0.0661 0.0126 1.0000
7.500 1.2167 0.01447 0.00741 -0.0649 0.0115 1.0000
7.750 1.2365 0.01484 0.00781 -0.0636 0.0103 1.0000
8.000 1.2556 0.01524 0.00825 -0.0621 0.0093 1.0000
8.250 1.2752 0.01559 0.00862 -0.0608 0.0088 1.0000
8.500 1.2940 0.01597 0.00903 -0.0594 0.0083 1.0000
8.750 1.3120 0.01637 0.00946 -0.0578 0.0077 1.0000
9.000 1.3289 0.01683 0.00996 -0.0561 0.0072 1.0000
9.250 1.3445 0.01735 0.01051 -0.0542 0.0067 1.0000
9.500 1.3608 0.01780 0.01100 -0.0525 0.0064 1.0000
9.750 1.3751 0.01831 0.01154 -0.0504 0.0061 1.0000
10.000 1.3864 0.01884 0.01212 -0.0478 0.0058 1.0000
10.250 1.3978 0.01943 0.01275 -0.0454 0.0056 1.0000
10.500 1.4093 0.02010 0.01346 -0.0431 0.0054 1.0000
10.750 1.4200 0.02087 0.01428 -0.0410 0.0052 1.0000
11.000 1.4287 0.02184 0.01531 -0.0388 0.0049 1.0000
11.250 1.4369 0.02293 0.01647 -0.0368 0.0048 1.0000
11.500 1.4470 0.02396 0.01756 -0.0351 0.0047 1.0000
11.750 1.4564 0.02512 0.01879 -0.0337 0.0045 1.0000
12.000 1.4654 0.02638 0.02012 -0.0324 0.0043 1.0000
12.250 1.4736 0.02781 0.02162 -0.0312 0.0042 1.0000
12.500 1.4813 0.02937 0.02325 -0.0303 0.0040 1.0000
12.750 1.4885 0.03106 0.02501 -0.0295 0.0039 1.0000
13.000 1.4945 0.03295 0.02697 -0.0288 0.0038 1.0000
13.250 1.5000 0.03495 0.02904 -0.0283 0.0037 1.0000
13.500 1.5045 0.03709 0.03125 -0.0278 0.0036 1.0000
13.750 1.5073 0.03943 0.03367 -0.0274 0.0035 1.0000
14.000 1.5083 0.04201 0.03632 -0.0270 0.0035 1.0000
14.250 1.5068 0.04488 0.03930 -0.0266 0.0034 1.0000
14.500 1.5023 0.04817 0.04269 -0.0264 0.0033 1.0000
14.750 1.4967 0.05166 0.04628 -0.0263 0.0032 1.0000
15.000 1.4948 0.05481 0.04952 -0.0263 0.0032 1.0000
15.250 1.4916 0.05820 0.05301 -0.0265 0.0032 1.0000
15.500 1.4878 0.06175 0.05666 -0.0268 0.0031 1.0000
15.750 1.4831 0.06547 0.06048 -0.0273 0.0031 1.0000
16.000 1.4777 0.06939 0.06449 -0.0278 0.0031 1.0000
16.250 1.4715 0.07349 0.06869 -0.0285 0.0030 1.0000
16.500 1.4645 0.07772 0.07302 -0.0293 0.0030 1.0000
16.750 1.4570 0.08210 0.07750 -0.0302 0.0030 1.0000
17.000 1.4488 0.08668 0.08218 -0.0312 0.0029 1.0000
17.250 1.4402 0.09138 0.08698 -0.0323 0.0029 1.0000
17.500 1.4309 0.09621 0.09191 -0.0336 0.0029 1.0000
17.750 1.4210 0.10123 0.09704 -0.0350 0.0029 1.0000
18.000 1.4115 0.10628 0.10218 -0.0365 0.0028 1.0000
18.250 1.4007 0.11163 0.10763 -0.0382 0.0028 1.0000
18.500 1.3902 0.11698 0.11308 -0.0400 0.0028 1.0000
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Polar data table (+)
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