Dayton-Wright 6 (daytonwright6-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Dayton-Wright 6 (daytonwright6-il) Reynolds number: 1,000,000 Max Cl/Cd: 111.24 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-daytonwright6-il-1000000-n5.txt Download as CSV file: xf-daytonwright6-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Dayton-Wright 6
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 -0.7608 0.03508 0.03244 -0.1174 0.9862 0.0202
-14.500 -0.7604 0.03223 0.02940 -0.1179 0.9804 0.0203
-14.250 -0.7521 0.03035 0.02739 -0.1173 0.9740 0.0204
-14.000 -0.7450 0.02851 0.02540 -0.1160 0.9656 0.0205
-13.500 -0.7111 0.02557 0.02218 -0.1154 0.9511 0.0208
-13.250 -0.6842 0.02419 0.02066 -0.1167 0.9449 0.0210
-13.000 -0.6524 0.02292 0.01924 -0.1187 0.9357 0.0212
-12.750 -0.6117 0.02165 0.01781 -0.1226 0.9276 0.0214
-12.500 -0.5726 0.02050 0.01646 -0.1259 0.9153 0.0217
-12.250 -0.5411 0.01947 0.01524 -0.1275 0.8976 0.0219
-12.000 -0.5178 0.01869 0.01426 -0.1271 0.8785 0.0220
-11.750 -0.4985 0.01807 0.01348 -0.1257 0.8625 0.0222
-11.500 -0.4797 0.01758 0.01283 -0.1241 0.8491 0.0223
-11.250 -0.4615 0.01702 0.01214 -0.1223 0.8381 0.0224
-11.000 -0.4424 0.01650 0.01149 -0.1207 0.8294 0.0225
-10.750 -0.4222 0.01608 0.01097 -0.1192 0.8215 0.0226
-10.500 -0.4016 0.01562 0.01041 -0.1177 0.8157 0.0227
-10.250 -0.3804 0.01519 0.00990 -0.1164 0.8096 0.0228
-10.000 -0.3586 0.01483 0.00944 -0.1151 0.8038 0.0229
-9.750 -0.3378 0.01429 0.00881 -0.1137 0.7990 0.0231
-9.500 -0.3183 0.01361 0.00806 -0.1121 0.7934 0.0234
-9.250 -0.2965 0.01321 0.00759 -0.1108 0.7876 0.0237
-9.000 -0.2742 0.01282 0.00713 -0.1096 0.7819 0.0238
-8.750 -0.2513 0.01248 0.00675 -0.1085 0.7753 0.0240
-8.500 -0.2286 0.01219 0.00639 -0.1073 0.7686 0.0242
-8.250 -0.2050 0.01189 0.00605 -0.1062 0.7614 0.0243
-8.000 -0.1824 0.01164 0.00572 -0.1050 0.7523 0.0245
-7.750 -0.1590 0.01139 0.00542 -0.1039 0.7414 0.0247
-7.500 -0.1367 0.01117 0.00512 -0.1026 0.7263 0.0249
-7.250 -0.1160 0.01100 0.00484 -0.1009 0.7015 0.0251
-7.000 -0.0980 0.01095 0.00460 -0.0986 0.6601 0.0253
-6.750 -0.0792 0.01093 0.00439 -0.0965 0.6230 0.0255
-6.500 -0.0580 0.01084 0.00417 -0.0950 0.5986 0.0257
-6.250 -0.0355 0.01073 0.00397 -0.0937 0.5814 0.0260
-6.000 -0.0126 0.01062 0.00378 -0.0925 0.5672 0.0262
-5.750 0.0107 0.01052 0.00360 -0.0914 0.5551 0.0265
-5.500 0.0343 0.01041 0.00343 -0.0904 0.5439 0.0267
-5.250 0.0583 0.01031 0.00327 -0.0894 0.5347 0.0269
-5.000 0.0823 0.01022 0.00312 -0.0884 0.5263 0.0272
-4.750 0.1068 0.01013 0.00299 -0.0876 0.5193 0.0274
-4.500 0.1311 0.01004 0.00287 -0.0867 0.5120 0.0277
-4.250 0.1548 0.00991 0.00269 -0.0857 0.5048 0.0283
-4.000 0.1792 0.00979 0.00255 -0.0848 0.4988 0.0290
-3.750 0.2033 0.00972 0.00244 -0.0839 0.4929 0.0296
-3.500 0.2279 0.00965 0.00235 -0.0831 0.4877 0.0300
-3.250 0.2526 0.00959 0.00227 -0.0823 0.4819 0.0306
-3.000 0.2765 0.00956 0.00220 -0.0814 0.4750 0.0313
-2.750 0.3012 0.00951 0.00214 -0.0806 0.4692 0.0320
-2.500 0.3258 0.00948 0.00208 -0.0798 0.4634 0.0328
-2.000 0.3741 0.00941 0.00199 -0.0780 0.4524 0.0376
-1.750 0.3966 0.00926 0.00195 -0.0769 0.4462 0.0667
-1.500 0.4199 0.00925 0.00194 -0.0759 0.4394 0.0781
-1.250 0.4437 0.00923 0.00193 -0.0750 0.4321 0.0891
-1.000 0.4667 0.00924 0.00194 -0.0740 0.4251 0.0997
-0.500 0.5133 0.00922 0.00197 -0.0720 0.4116 0.1279
-0.250 0.5360 0.00921 0.00200 -0.0710 0.4050 0.1479
0.000 0.5584 0.00922 0.00203 -0.0698 0.3969 0.1677
0.250 0.5805 0.00925 0.00207 -0.0687 0.3886 0.1855
0.500 0.6018 0.00926 0.00212 -0.0673 0.3808 0.2124
0.750 0.6219 0.00925 0.00217 -0.0658 0.3743 0.2480
1.000 0.6408 0.00916 0.00224 -0.0640 0.3679 0.3147
1.250 0.6580 0.00907 0.00232 -0.0619 0.3616 0.3980
1.750 0.8284 0.00859 0.00322 -0.0883 0.3414 0.9795
2.000 0.8685 0.00882 0.00340 -0.0912 0.3349 0.9871
2.250 0.9018 0.00902 0.00355 -0.0927 0.3291 0.9904
2.500 0.9338 0.00918 0.00368 -0.0938 0.3242 0.9932
2.750 0.9927 0.00938 0.00382 -0.1010 0.3178 0.9979
3.000 1.0356 0.00953 0.00393 -0.1047 0.3124 1.0000
3.250 1.0558 0.00964 0.00403 -0.1033 0.3090 1.0000
3.500 1.0756 0.00976 0.00415 -0.1018 0.3051 1.0000
3.750 1.0945 0.00992 0.00428 -0.1002 0.3010 1.0000
4.000 1.1133 0.01007 0.00441 -0.0985 0.2962 1.0000
4.250 1.1330 0.01019 0.00454 -0.0970 0.2933 1.0000
4.500 1.1513 0.01035 0.00468 -0.0953 0.2879 1.0000
4.750 1.1680 0.01054 0.00484 -0.0932 0.2826 1.0000
5.000 1.1844 0.01067 0.00497 -0.0911 0.2787 1.0000
5.250 1.1999 0.01080 0.00511 -0.0888 0.2743 1.0000
5.500 1.2138 0.01102 0.00529 -0.0862 0.2674 1.0000
5.750 1.2306 0.01117 0.00544 -0.0842 0.2627 1.0000
6.000 1.2460 0.01138 0.00563 -0.0820 0.2557 1.0000
6.250 1.2619 0.01160 0.00584 -0.0799 0.2505 1.0000
6.500 1.2783 0.01182 0.00604 -0.0780 0.2428 1.0000
6.750 1.2933 0.01210 0.00629 -0.0759 0.2359 1.0000
7.000 1.3088 0.01238 0.00655 -0.0739 0.2262 1.0000
7.250 1.3235 0.01271 0.00685 -0.0718 0.2170 1.0000
7.500 1.3359 0.01315 0.00722 -0.0693 0.2032 1.0000
7.750 1.3460 0.01371 0.00768 -0.0666 0.1856 1.0000
8.000 1.3480 0.01464 0.00842 -0.0626 0.1562 1.0000
8.250 1.3525 0.01550 0.00915 -0.0591 0.1344 1.0000
8.500 1.3481 0.01683 0.01027 -0.0545 0.1017 1.0000
8.750 1.3212 0.01941 0.01250 -0.0471 0.0418 1.0000
9.000 1.3168 0.02103 0.01404 -0.0432 0.0174 1.0000
9.250 1.3270 0.02189 0.01491 -0.0415 0.0153 1.0000
9.500 1.3374 0.02277 0.01582 -0.0398 0.0140 1.0000
9.750 1.3486 0.02364 0.01673 -0.0384 0.0133 1.0000
10.000 1.3591 0.02459 0.01772 -0.0370 0.0126 1.0000
10.250 1.3687 0.02563 0.01880 -0.0356 0.0122 1.0000
10.500 1.3768 0.02682 0.02003 -0.0341 0.0116 1.0000
10.750 1.3840 0.02811 0.02137 -0.0327 0.0108 1.0000
11.000 1.3924 0.02936 0.02267 -0.0315 0.0106 1.0000
11.250 1.3999 0.03072 0.02408 -0.0304 0.0104 1.0000
11.500 1.4070 0.03217 0.02558 -0.0293 0.0101 1.0000
11.750 1.4130 0.03376 0.02724 -0.0283 0.0098 1.0000
12.000 1.4176 0.03553 0.02906 -0.0274 0.0095 1.0000
12.250 1.4215 0.03744 0.03102 -0.0266 0.0092 1.0000
12.500 1.4247 0.03951 0.03315 -0.0259 0.0090 1.0000
12.750 1.4254 0.04192 0.03563 -0.0253 0.0087 1.0000
13.000 1.4248 0.04455 0.03835 -0.0248 0.0085 1.0000
13.250 1.4243 0.04727 0.04114 -0.0245 0.0083 1.0000
13.500 1.4255 0.04991 0.04385 -0.0244 0.0082 1.0000
13.750 1.4256 0.05270 0.04671 -0.0244 0.0080 1.0000
14.000 1.4243 0.05570 0.04979 -0.0244 0.0079 1.0000
14.250 1.4209 0.05899 0.05317 -0.0245 0.0078 1.0000
14.500 1.4178 0.06231 0.05656 -0.0247 0.0077 1.0000
14.750 1.4112 0.06612 0.06047 -0.0250 0.0076 1.0000
15.000 1.4079 0.06951 0.06393 -0.0254 0.0075 1.0000
15.250 1.4013 0.07340 0.06791 -0.0259 0.0073 1.0000
15.500 1.3949 0.07732 0.07191 -0.0264 0.0072 1.0000
15.750 1.3875 0.08144 0.07611 -0.0271 0.0071 1.0000
16.000 1.3794 0.08568 0.08044 -0.0278 0.0070 1.0000
16.250 1.3735 0.08968 0.08452 -0.0286 0.0069 1.0000
16.500 1.3647 0.09418 0.08910 -0.0295 0.0068 1.0000
16.750 1.3566 0.09861 0.09360 -0.0306 0.0067 1.0000
17.000 1.3490 0.10297 0.09804 -0.0316 0.0067 1.0000
17.250 1.3393 0.10771 0.10286 -0.0328 0.0065 1.0000
17.500 1.3303 0.11240 0.10764 -0.0341 0.0065 1.0000
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