EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il) Reynolds number: 1,000,000 Max Cl/Cd: 64.01 at α=10.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ea61012-il-1000000.txt Download as CSV file: xf-ea61012-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: EPPLER EA 6(-1)-012 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3506 0.08799 0.08488 -0.0174 1.0000 0.0188
-19.500 -1.3765 0.07986 0.07659 -0.0221 1.0000 0.0188
-19.250 -1.3947 0.07320 0.06978 -0.0257 1.0000 0.0190
-19.000 -1.4140 0.06659 0.06303 -0.0293 1.0000 0.0192
-18.750 -1.4321 0.06048 0.05680 -0.0324 1.0000 0.0196
-18.500 -1.4431 0.05576 0.05198 -0.0345 1.0000 0.0199
-18.250 -1.4486 0.05199 0.04813 -0.0359 1.0000 0.0203
-18.000 -1.4508 0.04883 0.04490 -0.0368 1.0000 0.0208
-17.750 -1.4506 0.04612 0.04211 -0.0374 1.0000 0.0213
-17.500 -1.4500 0.04353 0.03943 -0.0378 1.0000 0.0217
-17.250 -1.4449 0.04151 0.03731 -0.0379 1.0000 0.0222
-17.000 -1.4396 0.03955 0.03525 -0.0380 1.0000 0.0226
-16.750 -1.4421 0.03690 0.03252 -0.0379 1.0000 0.0232
-16.500 -1.4364 0.03512 0.03072 -0.0377 1.0000 0.0239
-16.250 -1.4283 0.03361 0.02916 -0.0373 1.0000 0.0245
-16.000 -1.4166 0.03245 0.02796 -0.0369 1.0000 0.0252
-15.750 -1.4060 0.03123 0.02667 -0.0364 1.0000 0.0257
-15.500 -1.3941 0.03014 0.02551 -0.0359 1.0000 0.0263
-15.250 -1.3811 0.02916 0.02445 -0.0353 1.0000 0.0266
-15.000 -1.3775 0.02748 0.02271 -0.0342 1.0000 0.0274
-14.750 -1.3662 0.02646 0.02166 -0.0334 1.0000 0.0281
-14.500 -1.3526 0.02564 0.02082 -0.0326 1.0000 0.0287
-14.250 -1.3378 0.02493 0.02008 -0.0318 1.0000 0.0293
-14.000 -1.3224 0.02430 0.01941 -0.0310 1.0000 0.0300
-13.750 -1.3082 0.02360 0.01865 -0.0300 1.0000 0.0305
-13.500 -1.2913 0.02314 0.01812 -0.0291 1.0000 0.0311
-13.250 -1.2774 0.02250 0.01741 -0.0278 1.0000 0.0314
-13.000 -1.2714 0.02136 0.01623 -0.0255 1.0000 0.0322
-12.750 -1.2581 0.02081 0.01567 -0.0238 1.0000 0.0328
-12.500 -1.2430 0.02041 0.01525 -0.0222 1.0000 0.0334
-12.250 -1.2267 0.02008 0.01490 -0.0205 1.0000 0.0340
-12.000 -1.2090 0.01975 0.01454 -0.0191 1.0000 0.0347
-11.750 -1.1890 0.01943 0.01418 -0.0181 1.0000 0.0354
-11.500 -1.1689 0.01906 0.01376 -0.0171 1.0000 0.0359
-11.250 -1.1478 0.01874 0.01339 -0.0162 1.0000 0.0364
-11.000 -1.1280 0.01822 0.01282 -0.0152 1.0000 0.0369
-10.750 -1.1113 0.01737 0.01195 -0.0138 1.0000 0.0379
-10.500 -1.0892 0.01705 0.01164 -0.0131 1.0000 0.0387
-10.250 -1.0666 0.01673 0.01132 -0.0124 1.0000 0.0394
-10.000 -1.0437 0.01641 0.01099 -0.0118 1.0000 0.0401
-9.750 -1.0204 0.01611 0.01067 -0.0112 1.0000 0.0409
-9.500 -0.9908 0.01576 0.01029 -0.0119 0.9703 0.0417
-9.250 -0.9468 0.01553 0.00989 -0.0155 0.9016 0.0424
-9.000 -0.9247 0.01542 0.00962 -0.0144 0.8717 0.0428
-8.750 -0.9070 0.01455 0.00865 -0.0130 0.8582 0.0438
-8.500 -0.8852 0.01408 0.00813 -0.0121 0.8496 0.0447
-8.250 -0.8614 0.01379 0.00781 -0.0115 0.8425 0.0456
-8.000 -0.8372 0.01352 0.00750 -0.0109 0.8366 0.0463
-7.750 -0.8126 0.01322 0.00717 -0.0104 0.8314 0.0471
-7.500 -0.7879 0.01294 0.00684 -0.0098 0.8264 0.0479
-7.250 -0.7630 0.01269 0.00654 -0.0093 0.8215 0.0487
-7.000 -0.7372 0.01246 0.00630 -0.0090 0.8173 0.0494
-6.750 -0.7111 0.01228 0.00608 -0.0087 0.8129 0.0499
-6.500 -0.6880 0.01178 0.00552 -0.0079 0.8085 0.0510
-6.250 -0.6637 0.01139 0.00511 -0.0073 0.8044 0.0524
-6.000 -0.6380 0.01110 0.00482 -0.0070 0.8007 0.0536
-5.750 -0.6118 0.01087 0.00457 -0.0066 0.7968 0.0547
-5.500 -0.5855 0.01066 0.00434 -0.0063 0.7930 0.0559
-5.250 -0.5590 0.01050 0.00414 -0.0060 0.7890 0.0571
-5.000 -0.5320 0.01032 0.00395 -0.0058 0.7856 0.0580
-4.750 -0.5053 0.01009 0.00371 -0.0056 0.7817 0.0591
-4.500 -0.4793 0.00980 0.00341 -0.0052 0.7779 0.0616
-4.250 -0.4527 0.00961 0.00321 -0.0049 0.7739 0.0638
-4.000 -0.4255 0.00943 0.00303 -0.0047 0.7697 0.0659
-3.750 -0.3980 0.00928 0.00287 -0.0045 0.7649 0.0679
-3.500 -0.3713 0.00906 0.00267 -0.0043 0.7602 0.0732
-3.250 -0.3442 0.00890 0.00251 -0.0040 0.7559 0.0791
-3.000 -0.3179 0.00856 0.00232 -0.0037 0.7516 0.1041
-2.750 -0.2937 0.00799 0.00208 -0.0032 0.7470 0.1800
-2.500 -0.2693 0.00748 0.00186 -0.0027 0.7427 0.2560
-2.250 -0.2452 0.00693 0.00168 -0.0022 0.7386 0.3535
-2.000 -0.2192 0.00655 0.00154 -0.0019 0.7341 0.4136
-1.750 -0.1954 0.00599 0.00138 -0.0012 0.7292 0.5190
-1.500 -0.1686 0.00581 0.00134 -0.0009 0.7246 0.5744
-1.250 -0.1406 0.00572 0.00132 -0.0008 0.7204 0.5988
-1.000 -0.1124 0.00564 0.00130 -0.0007 0.7141 0.6178
-0.500 -0.0564 0.00554 0.00125 -0.0003 0.6966 0.6520
-0.250 -0.0283 0.00552 0.00122 -0.0001 0.6857 0.6632
0.000 0.0000 0.00552 0.00121 0.0000 0.6750 0.6751
0.250 0.0282 0.00552 0.00122 0.0002 0.6630 0.6858
0.500 0.0563 0.00554 0.00125 0.0003 0.6520 0.6966
0.750 0.0845 0.00561 0.00127 0.0005 0.6369 0.7066
1.000 0.1123 0.00565 0.00130 0.0007 0.6177 0.7143
1.250 0.1405 0.00572 0.00132 0.0008 0.5987 0.7204
1.500 0.1685 0.00581 0.00134 0.0009 0.5743 0.7247
1.750 0.1953 0.00599 0.00138 0.0013 0.5186 0.7292
2.000 0.2192 0.00655 0.00154 0.0019 0.4135 0.7340
2.250 0.2452 0.00693 0.00168 0.0022 0.3543 0.7386
2.500 0.2693 0.00747 0.00186 0.0027 0.2570 0.7427
2.750 0.2937 0.00799 0.00208 0.0032 0.1807 0.7470
3.000 0.3179 0.00856 0.00232 0.0037 0.1041 0.7517
3.250 0.3442 0.00890 0.00251 0.0040 0.0790 0.7559
3.500 0.3712 0.00906 0.00267 0.0043 0.0731 0.7602
3.750 0.3980 0.00928 0.00287 0.0046 0.0679 0.7649
4.000 0.4254 0.00943 0.00303 0.0047 0.0659 0.7698
4.250 0.4526 0.00961 0.00321 0.0049 0.0638 0.7739
4.500 0.4792 0.00980 0.00341 0.0052 0.0616 0.7779
4.750 0.5053 0.01009 0.00371 0.0056 0.0591 0.7817
5.000 0.5319 0.01032 0.00395 0.0059 0.0580 0.7856
5.250 0.5589 0.01050 0.00414 0.0061 0.0571 0.7890
5.500 0.5855 0.01066 0.00434 0.0063 0.0558 0.7930
5.750 0.6118 0.01087 0.00457 0.0067 0.0547 0.7968
6.000 0.6379 0.01110 0.00482 0.0070 0.0536 0.8007
6.250 0.6637 0.01139 0.00510 0.0073 0.0524 0.8044
6.500 0.6880 0.01178 0.00551 0.0079 0.0511 0.8085
6.750 0.7110 0.01228 0.00608 0.0087 0.0499 0.8129
7.000 0.7371 0.01246 0.00629 0.0090 0.0494 0.8173
7.250 0.7629 0.01270 0.00655 0.0094 0.0487 0.8215
7.500 0.7878 0.01294 0.00685 0.0099 0.0479 0.8264
7.750 0.8125 0.01322 0.00717 0.0104 0.0472 0.8314
8.000 0.8372 0.01351 0.00749 0.0109 0.0463 0.8366
8.250 0.8613 0.01380 0.00781 0.0115 0.0456 0.8425
8.500 0.8851 0.01408 0.00813 0.0121 0.0447 0.8496
8.750 0.9068 0.01456 0.00865 0.0130 0.0438 0.8583
9.000 0.9245 0.01542 0.00962 0.0145 0.0428 0.8719
9.250 0.9468 0.01551 0.00987 0.0155 0.0424 0.9022
9.500 0.9912 0.01576 0.01029 0.0118 0.0417 0.9713
9.750 1.0203 0.01612 0.01068 0.0112 0.0409 1.0000
10.000 1.0438 0.01641 0.01098 0.0118 0.0401 1.0000
10.250 1.0667 0.01671 0.01130 0.0124 0.0394 1.0000
10.500 1.0895 0.01702 0.01161 0.0131 0.0387 1.0000
10.750 1.1113 0.01738 0.01197 0.0139 0.0379 1.0000
11.000 1.1278 0.01826 0.01286 0.0152 0.0369 1.0000
11.250 1.1473 0.01881 0.01346 0.0163 0.0364 1.0000
11.500 1.1691 0.01905 0.01375 0.0171 0.0359 1.0000
11.750 1.1893 0.01941 0.01416 0.0181 0.0353 1.0000
12.000 1.2094 0.01973 0.01452 0.0191 0.0347 1.0000
12.250 1.2279 0.02001 0.01482 0.0204 0.0339 1.0000
12.500 1.2435 0.02039 0.01523 0.0221 0.0334 1.0000
12.750 1.2587 0.02079 0.01565 0.0237 0.0328 1.0000
13.000 1.2717 0.02137 0.01624 0.0255 0.0322 1.0000
13.250 1.2777 0.02250 0.01741 0.0277 0.0314 1.0000
13.500 1.2920 0.02312 0.01810 0.0290 0.0310 1.0000
13.750 1.3080 0.02365 0.01869 0.0300 0.0305 1.0000
14.000 1.3222 0.02435 0.01945 0.0310 0.0300 1.0000
14.250 1.3383 0.02493 0.02007 0.0318 0.0293 1.0000
14.500 1.3514 0.02576 0.02096 0.0327 0.0288 1.0000
14.750 1.3670 0.02642 0.02163 0.0333 0.0281 1.0000
15.000 1.3780 0.02748 0.02271 0.0342 0.0274 1.0000
15.250 1.3812 0.02920 0.02448 0.0352 0.0267 1.0000
15.500 1.3949 0.03013 0.02549 0.0358 0.0263 1.0000
15.750 1.4065 0.03125 0.02669 0.0363 0.0258 1.0000
16.000 1.4175 0.03243 0.02794 0.0368 0.0252 1.0000
16.250 1.4284 0.03366 0.02922 0.0372 0.0245 1.0000
16.500 1.4371 0.03513 0.03073 0.0375 0.0239 1.0000
16.750 1.4422 0.03697 0.03261 0.0378 0.0233 1.0000
17.000 1.4420 0.03940 0.03510 0.0378 0.0225 1.0000
17.250 1.4475 0.04134 0.03713 0.0378 0.0222 1.0000
17.500 1.4507 0.04357 0.03946 0.0376 0.0218 1.0000
17.750 1.4530 0.04598 0.04196 0.0372 0.0213 1.0000
18.000 1.4530 0.04873 0.04479 0.0366 0.0207 1.0000
18.250 1.4504 0.05193 0.04806 0.0357 0.0203 1.0000
18.500 1.4445 0.05577 0.05199 0.0342 0.0199 1.0000
18.750 1.4319 0.06074 0.05705 0.0320 0.0194 1.0000
19.000 1.4159 0.06653 0.06297 0.0291 0.0192 1.0000
19.250 1.3969 0.07312 0.06970 0.0255 0.0190 1.0000
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