RG 14 9% AIRFOIL (rg149-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: RG 14 9% AIRFOIL (rg149-il) Reynolds number: 1,000,000 Max Cl/Cd: 84.18 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rg149-il-1000000-n5.txt Download as CSV file: xf-rg149-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: RG 14 9% 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
------ -------- --------- --------- -------- -------- --------
-14.250 -1.0345 0.04594 0.04366 -0.0570 1.0000 0.0035
-14.000 -1.0616 0.03921 0.03671 -0.0617 1.0000 0.0035
-13.750 -1.0851 0.03513 0.03241 -0.0613 1.0000 0.0034
-13.500 -1.0977 0.03286 0.03000 -0.0584 1.0000 0.0035
-13.250 -1.1014 0.03117 0.02817 -0.0554 1.0000 0.0035
-13.000 -1.0998 0.02937 0.02621 -0.0531 1.0000 0.0036
-12.750 -1.0936 0.02784 0.02453 -0.0511 1.0000 0.0036
-12.500 -1.0849 0.02641 0.02296 -0.0492 1.0000 0.0037
-12.250 -1.0748 0.02505 0.02145 -0.0473 1.0000 0.0038
-12.000 -1.0625 0.02385 0.02011 -0.0455 1.0000 0.0039
-11.750 -1.0488 0.02275 0.01887 -0.0438 1.0000 0.0040
-11.500 -1.0329 0.02186 0.01787 -0.0423 1.0000 0.0042
-11.250 -1.0165 0.02100 0.01690 -0.0408 1.0000 0.0043
-11.000 -1.0002 0.02007 0.01585 -0.0393 1.0000 0.0044
-10.750 -0.9831 0.01923 0.01487 -0.0378 1.0000 0.0045
-10.500 -0.9649 0.01851 0.01404 -0.0364 1.0000 0.0046
-10.250 -0.9470 0.01770 0.01313 -0.0349 1.0000 0.0047
-10.000 -0.9298 0.01675 0.01205 -0.0333 1.0000 0.0051
-9.750 -0.9088 0.01607 0.01129 -0.0324 0.9998 0.0053
-9.500 -0.8797 0.01544 0.01059 -0.0331 0.9988 0.0057
-9.250 -0.8499 0.01493 0.01002 -0.0339 0.9975 0.0060
-9.000 -0.8197 0.01439 0.00940 -0.0348 0.9962 0.0064
-8.750 -0.7891 0.01386 0.00880 -0.0357 0.9950 0.0068
-8.500 -0.7586 0.01339 0.00825 -0.0366 0.9937 0.0071
-8.250 -0.7302 0.01284 0.00763 -0.0370 0.9917 0.0076
-8.000 -0.7003 0.01246 0.00725 -0.0376 0.9896 0.0083
-7.750 -0.6696 0.01214 0.00691 -0.0385 0.9877 0.0090
-7.500 -0.6379 0.01187 0.00660 -0.0395 0.9860 0.0098
-7.250 -0.6055 0.01159 0.00628 -0.0406 0.9845 0.0105
-7.000 -0.5728 0.01120 0.00585 -0.0418 0.9832 0.0110
-6.750 -0.5469 0.01079 0.00542 -0.0415 0.9788 0.0119
-6.500 -0.5169 0.01050 0.00512 -0.0421 0.9754 0.0127
-6.250 -0.4851 0.01022 0.00480 -0.0430 0.9727 0.0135
-6.000 -0.4525 0.00995 0.00451 -0.0441 0.9703 0.0143
-5.750 -0.4256 0.00971 0.00424 -0.0439 0.9638 0.0149
-5.500 -0.3941 0.00946 0.00396 -0.0448 0.9591 0.0153
-5.250 -0.3635 0.00906 0.00352 -0.0454 0.9533 0.0164
-5.000 -0.3324 0.00874 0.00316 -0.0462 0.9456 0.0176
-4.750 -0.3013 0.00849 0.00287 -0.0469 0.9361 0.0186
-4.500 -0.2709 0.00827 0.00262 -0.0474 0.9247 0.0198
-4.250 -0.2422 0.00810 0.00239 -0.0475 0.9112 0.0206
-4.000 -0.2146 0.00796 0.00217 -0.0473 0.8962 0.0213
-3.750 -0.1876 0.00782 0.00197 -0.0470 0.8806 0.0233
-3.500 -0.1611 0.00768 0.00180 -0.0467 0.8643 0.0271
-3.250 -0.1349 0.00754 0.00164 -0.0462 0.8474 0.0371
-3.000 -0.1088 0.00740 0.00150 -0.0458 0.8296 0.0531
-2.750 -0.0828 0.00728 0.00137 -0.0454 0.8115 0.0702
-2.500 -0.0568 0.00715 0.00126 -0.0450 0.7929 0.0931
-2.250 -0.0308 0.00702 0.00116 -0.0446 0.7744 0.1199
-2.000 -0.0048 0.00691 0.00107 -0.0442 0.7556 0.1484
-1.750 0.0212 0.00676 0.00100 -0.0438 0.7371 0.1896
-1.250 0.0730 0.00652 0.00088 -0.0431 0.6970 0.2733
-1.000 0.0983 0.00634 0.00083 -0.0427 0.6724 0.3398
-0.750 0.1228 0.00619 0.00080 -0.0421 0.6408 0.4180
-0.500 0.1473 0.00594 0.00077 -0.0416 0.6136 0.5162
-0.250 0.1726 0.00574 0.00076 -0.0411 0.5948 0.5983
0.000 0.1977 0.00557 0.00076 -0.0406 0.5753 0.6749
0.250 0.2228 0.00546 0.00081 -0.0399 0.5562 0.7455
0.500 0.2487 0.00550 0.00086 -0.0394 0.5343 0.7834
0.750 0.2745 0.00559 0.00092 -0.0389 0.5075 0.8083
1.000 0.3010 0.00568 0.00097 -0.0386 0.4856 0.8248
1.250 0.3276 0.00577 0.00102 -0.0382 0.4671 0.8369
1.500 0.3542 0.00587 0.00108 -0.0379 0.4461 0.8484
1.750 0.3802 0.00601 0.00115 -0.0375 0.4202 0.8607
2.000 0.4060 0.00618 0.00124 -0.0370 0.3919 0.8722
2.250 0.4314 0.00638 0.00133 -0.0365 0.3566 0.8820
2.500 0.4565 0.00660 0.00144 -0.0359 0.3219 0.8921
2.750 0.4815 0.00679 0.00155 -0.0353 0.2934 0.9038
3.000 0.5063 0.00696 0.00167 -0.0346 0.2686 0.9166
3.250 0.5308 0.00714 0.00179 -0.0339 0.2453 0.9298
3.750 0.5797 0.00768 0.00211 -0.0325 0.1788 0.9522
4.000 0.6066 0.00793 0.00227 -0.0324 0.1573 0.9609
4.250 0.6347 0.00816 0.00244 -0.0326 0.1416 0.9698
4.500 0.6654 0.00840 0.00262 -0.0333 0.1268 0.9767
4.750 0.6957 0.00864 0.00280 -0.0340 0.1099 0.9840
5.000 0.7273 0.00890 0.00300 -0.0350 0.0946 0.9902
5.250 0.7582 0.00917 0.00321 -0.0359 0.0819 0.9973
5.500 0.7850 0.00943 0.00343 -0.0358 0.0726 1.0000
5.750 0.8093 0.00967 0.00366 -0.0352 0.0651 1.0000
6.000 0.8340 0.00991 0.00388 -0.0347 0.0592 1.0000
6.250 0.8584 0.01020 0.00414 -0.0341 0.0518 1.0000
6.500 0.8830 0.01049 0.00440 -0.0336 0.0443 1.0000
6.750 0.9073 0.01081 0.00468 -0.0330 0.0374 1.0000
7.000 0.9318 0.01111 0.00498 -0.0325 0.0328 1.0000
7.250 0.9562 0.01143 0.00529 -0.0320 0.0285 1.0000
7.500 0.9806 0.01174 0.00561 -0.0315 0.0255 1.0000
7.750 1.0045 0.01212 0.00596 -0.0309 0.0216 1.0000
8.000 1.0288 0.01243 0.00630 -0.0304 0.0199 1.0000
8.250 1.0524 0.01282 0.00669 -0.0298 0.0171 1.0000
8.500 1.0762 0.01318 0.00707 -0.0292 0.0151 1.0000
8.750 1.0990 0.01363 0.00751 -0.0285 0.0117 1.0000
9.000 1.1217 0.01408 0.00798 -0.0278 0.0094 1.0000
9.250 1.1438 0.01459 0.00850 -0.0270 0.0073 1.0000
9.500 1.1661 0.01506 0.00901 -0.0262 0.0065 1.0000
9.750 1.1876 0.01560 0.00960 -0.0253 0.0058 1.0000
10.000 1.2086 0.01618 0.01022 -0.0244 0.0051 1.0000
10.250 1.2295 0.01674 0.01085 -0.0234 0.0048 1.0000
10.500 1.2503 0.01727 0.01144 -0.0225 0.0046 1.0000
10.750 1.2705 0.01784 0.01208 -0.0215 0.0044 1.0000
11.000 1.2900 0.01845 0.01276 -0.0204 0.0042 1.0000
11.250 1.3086 0.01911 0.01351 -0.0192 0.0040 1.0000
11.500 1.3264 0.01978 0.01425 -0.0179 0.0038 1.0000
11.750 1.3431 0.02051 0.01505 -0.0164 0.0036 1.0000
12.000 1.3581 0.02132 0.01595 -0.0148 0.0035 1.0000
12.250 1.3703 0.02221 0.01692 -0.0127 0.0032 1.0000
12.500 1.3760 0.02333 0.01816 -0.0096 0.0030 1.0000
12.750 1.3830 0.02433 0.01926 -0.0069 0.0030 1.0000
13.000 1.3928 0.02515 0.02016 -0.0047 0.0029 1.0000
13.250 1.4002 0.02616 0.02126 -0.0024 0.0029 1.0000
13.500 1.4070 0.02723 0.02243 -0.0003 0.0028 1.0000
13.750 1.4115 0.02852 0.02384 0.0018 0.0028 1.0000
14.000 1.4145 0.02998 0.02541 0.0038 0.0027 1.0000
14.250 1.4185 0.03147 0.02700 0.0054 0.0026 1.0000
14.500 1.4180 0.03343 0.02908 0.0069 0.0026 1.0000
14.750 1.4162 0.03567 0.03145 0.0080 0.0026 1.0000
15.000 1.4148 0.03808 0.03396 0.0086 0.0025 1.0000
15.250 1.4094 0.04110 0.03712 0.0087 0.0025 1.0000
15.500 1.4026 0.04458 0.04074 0.0083 0.0024 1.0000
15.750 1.3947 0.04851 0.04480 0.0073 0.0024 1.0000
16.000 1.3841 0.05315 0.04958 0.0055 0.0024 1.0000
16.250 1.3733 0.05818 0.05474 0.0032 0.0024 1.0000
16.500 1.3526 0.06520 0.06194 -0.0005 0.0024 1.0000
16.750 1.3333 0.07245 0.06934 -0.0045 0.0023 1.0000
17.000 1.3070 0.08145 0.07851 -0.0097 0.0024 1.0000
17.250 1.2678 0.09355 0.09080 -0.0168 0.0024 1.0000
17.500 1.2270 0.10662 0.10406 -0.0244 0.0025 1.0000
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