NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63(3)-018 (naca633018-il) Reynolds number: 1,000,000 Max Cl/Cd: 83.05 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca633018-il-1000000.txt Download as CSV file: xf-naca633018-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(3)-018
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 -1.3187 0.08328 0.07909 -0.0153 1.0000 0.0164
-19.500 -1.3207 0.07963 0.07537 -0.0167 1.0000 0.0174
-19.250 -1.3233 0.07597 0.07168 -0.0181 1.0000 0.0187
-19.000 -1.3227 0.07281 0.06847 -0.0192 1.0000 0.0200
-18.750 -1.3203 0.06994 0.06554 -0.0201 1.0000 0.0211
-18.500 -1.3196 0.06688 0.06245 -0.0211 1.0000 0.0222
-18.250 -1.3158 0.06424 0.05978 -0.0219 1.0000 0.0234
-18.000 -1.3099 0.06191 0.05740 -0.0225 1.0000 0.0243
-17.750 -1.3025 0.05979 0.05521 -0.0231 1.0000 0.0250
-17.500 -1.2996 0.05715 0.05253 -0.0237 1.0000 0.0258
-17.250 -1.2962 0.05464 0.04998 -0.0242 1.0000 0.0266
-17.000 -1.2890 0.05257 0.04789 -0.0246 1.0000 0.0277
-16.750 -1.2801 0.05074 0.04603 -0.0249 1.0000 0.0286
-16.500 -1.2713 0.04890 0.04414 -0.0252 1.0000 0.0293
-16.250 -1.2638 0.04695 0.04213 -0.0254 1.0000 0.0297
-16.000 -1.2498 0.04568 0.04082 -0.0256 1.0000 0.0302
-15.750 -1.2490 0.04315 0.03823 -0.0257 1.0000 0.0311
-15.500 -1.2439 0.04110 0.03615 -0.0257 1.0000 0.0319
-15.250 -1.2362 0.03932 0.03435 -0.0257 1.0000 0.0327
-15.000 -1.2271 0.03771 0.03271 -0.0256 1.0000 0.0335
-14.750 -1.2171 0.03623 0.03119 -0.0254 1.0000 0.0341
-14.500 -1.2061 0.03487 0.02979 -0.0253 1.0000 0.0349
-14.250 -1.1947 0.03357 0.02845 -0.0250 1.0000 0.0355
-14.000 -1.1822 0.03237 0.02721 -0.0248 1.0000 0.0360
-13.750 -1.1698 0.03119 0.02599 -0.0245 1.0000 0.0363
-13.500 -1.1677 0.02923 0.02397 -0.0238 1.0000 0.0372
-13.250 -1.1613 0.02765 0.02236 -0.0231 1.0000 0.0383
-13.000 -1.1516 0.02636 0.02106 -0.0225 1.0000 0.0393
-12.750 -1.1404 0.02519 0.01988 -0.0219 1.0000 0.0401
-12.500 -1.1272 0.02419 0.01886 -0.0214 1.0000 0.0410
-12.250 -1.1138 0.02323 0.01787 -0.0208 1.0000 0.0419
-12.000 -1.0942 0.02228 0.01687 -0.0214 0.9604 0.0426
-11.750 -1.0612 0.02167 0.01610 -0.0240 0.9113 0.0434
-11.500 -1.0595 0.02047 0.01474 -0.0217 0.8797 0.0448
-11.250 -1.0528 0.01951 0.01370 -0.0198 0.8605 0.0462
-11.000 -1.0430 0.01870 0.01281 -0.0181 0.8457 0.0474
-10.750 -1.0319 0.01797 0.01202 -0.0165 0.8330 0.0486
-10.500 -1.0199 0.01731 0.01129 -0.0150 0.8220 0.0496
-10.250 -1.0061 0.01678 0.01068 -0.0135 0.8116 0.0508
-10.000 -0.9926 0.01625 0.01008 -0.0119 0.8022 0.0514
-9.750 -0.9846 0.01559 0.00934 -0.0094 0.7930 0.0533
-9.500 -0.9767 0.01500 0.00873 -0.0067 0.7840 0.0556
-9.250 -0.9655 0.01460 0.00829 -0.0042 0.7761 0.0577
-9.000 -0.9474 0.01423 0.00788 -0.0030 0.7686 0.0599
-8.750 -0.9288 0.01385 0.00746 -0.0017 0.7613 0.0634
-8.500 -0.9101 0.01340 0.00703 -0.0006 0.7544 0.0690
-8.250 -0.8903 0.01297 0.00661 0.0005 0.7474 0.0771
-8.000 -0.8707 0.01249 0.00618 0.0014 0.7410 0.0903
-7.750 -0.8503 0.01200 0.00576 0.0023 0.7343 0.1087
-7.500 -0.8303 0.01147 0.00533 0.0032 0.7278 0.1325
-7.250 -0.8090 0.01093 0.00493 0.0039 0.7217 0.1587
-7.000 -0.7874 0.01040 0.00453 0.0046 0.7156 0.1893
-6.750 -0.7656 0.00986 0.00413 0.0052 0.7098 0.2262
-6.500 -0.7430 0.00929 0.00375 0.0057 0.7038 0.2657
-6.250 -0.7196 0.00880 0.00341 0.0061 0.6977 0.3064
-6.000 -0.6951 0.00837 0.00313 0.0064 0.6921 0.3438
-5.750 -0.6689 0.00806 0.00293 0.0065 0.6865 0.3739
-5.500 -0.6419 0.00784 0.00276 0.0064 0.6808 0.3983
-5.250 -0.6140 0.00770 0.00264 0.0063 0.6754 0.4158
-5.000 -0.5856 0.00756 0.00253 0.0061 0.6697 0.4291
-4.750 -0.5572 0.00747 0.00242 0.0059 0.6640 0.4401
-4.500 -0.5283 0.00741 0.00234 0.0057 0.6589 0.4504
-4.250 -0.4995 0.00731 0.00226 0.0054 0.6537 0.4609
-4.000 -0.4707 0.00724 0.00218 0.0052 0.6482 0.4718
-3.750 -0.4417 0.00721 0.00212 0.0049 0.6429 0.4831
-3.500 -0.4126 0.00713 0.00208 0.0047 0.6377 0.4931
-3.250 -0.3832 0.00710 0.00201 0.0043 0.6326 0.4997
-3.000 -0.3543 0.00707 0.00197 0.0041 0.6275 0.5068
-2.750 -0.3245 0.00705 0.00193 0.0037 0.6227 0.5144
-2.500 -0.2954 0.00699 0.00189 0.0034 0.6174 0.5212
-2.250 -0.2660 0.00699 0.00185 0.0031 0.6123 0.5265
-2.000 -0.2363 0.00698 0.00182 0.0027 0.6079 0.5310
-1.750 -0.2069 0.00692 0.00178 0.0024 0.6029 0.5362
-1.500 -0.1775 0.00692 0.00175 0.0021 0.5979 0.5415
-1.250 -0.1477 0.00694 0.00174 0.0017 0.5932 0.5461
-1.000 -0.1183 0.00688 0.00172 0.0014 0.5886 0.5512
-0.750 -0.0888 0.00687 0.00170 0.0011 0.5838 0.5561
-0.500 -0.0593 0.00692 0.00169 0.0007 0.5787 0.5606
-0.250 -0.0295 0.00688 0.00168 0.0003 0.5746 0.5651
0.000 0.0000 0.00686 0.00168 0.0000 0.5699 0.5699
0.250 0.0295 0.00688 0.00168 -0.0003 0.5652 0.5746
0.500 0.0593 0.00692 0.00169 -0.0007 0.5606 0.5788
0.750 0.0888 0.00687 0.00170 -0.0011 0.5561 0.5838
1.000 0.1183 0.00688 0.00172 -0.0014 0.5512 0.5887
1.250 0.1477 0.00694 0.00174 -0.0017 0.5461 0.5932
1.500 0.1775 0.00692 0.00175 -0.0021 0.5415 0.5979
1.750 0.2069 0.00692 0.00178 -0.0024 0.5363 0.6029
2.000 0.2363 0.00698 0.00182 -0.0027 0.5310 0.6079
2.250 0.2660 0.00699 0.00185 -0.0031 0.5264 0.6123
2.500 0.2954 0.00699 0.00189 -0.0034 0.5212 0.6174
2.750 0.3245 0.00705 0.00193 -0.0037 0.5144 0.6227
3.000 0.3543 0.00707 0.00197 -0.0041 0.5068 0.6275
3.250 0.3832 0.00710 0.00201 -0.0043 0.4997 0.6326
3.500 0.4126 0.00713 0.00208 -0.0047 0.4933 0.6377
3.750 0.4417 0.00721 0.00212 -0.0049 0.4831 0.6429
4.000 0.4707 0.00724 0.00218 -0.0052 0.4718 0.6482
4.250 0.4995 0.00731 0.00226 -0.0054 0.4610 0.6537
4.500 0.5283 0.00741 0.00234 -0.0057 0.4505 0.6589
4.750 0.5572 0.00747 0.00242 -0.0059 0.4401 0.6640
5.000 0.5857 0.00756 0.00253 -0.0061 0.4291 0.6697
5.250 0.6140 0.00770 0.00264 -0.0063 0.4157 0.6755
5.500 0.6419 0.00784 0.00276 -0.0064 0.3980 0.6808
5.750 0.6689 0.00806 0.00293 -0.0065 0.3741 0.6865
6.000 0.6951 0.00837 0.00313 -0.0064 0.3438 0.6921
6.250 0.7196 0.00879 0.00341 -0.0061 0.3065 0.6977
6.500 0.7430 0.00929 0.00375 -0.0057 0.2656 0.7038
6.750 0.7656 0.00986 0.00413 -0.0052 0.2259 0.7097
7.000 0.7874 0.01040 0.00453 -0.0046 0.1893 0.7156
7.250 0.8090 0.01093 0.00493 -0.0039 0.1587 0.7217
7.500 0.8304 0.01147 0.00533 -0.0032 0.1324 0.7277
7.750 0.8503 0.01200 0.00576 -0.0023 0.1085 0.7343
8.000 0.8707 0.01249 0.00618 -0.0015 0.0904 0.7410
8.250 0.8904 0.01297 0.00661 -0.0005 0.0771 0.7474
8.500 0.9101 0.01340 0.00702 0.0006 0.0690 0.7543
8.750 0.9288 0.01386 0.00746 0.0017 0.0633 0.7613
9.000 0.9474 0.01423 0.00788 0.0029 0.0600 0.7686
9.250 0.9656 0.01460 0.00829 0.0042 0.0578 0.7761
9.500 0.9770 0.01500 0.00873 0.0066 0.0556 0.7840
9.750 0.9849 0.01558 0.00934 0.0094 0.0532 0.7930
10.000 0.9927 0.01625 0.01008 0.0119 0.0514 0.8023
10.250 1.0068 0.01676 0.01065 0.0134 0.0507 0.8115
10.500 1.0197 0.01733 0.01131 0.0150 0.0498 0.8219
10.750 1.0322 0.01796 0.01201 0.0165 0.0487 0.8329
11.000 1.0434 0.01868 0.01280 0.0181 0.0474 0.8457
11.500 1.0596 0.02047 0.01474 0.0216 0.0447 0.8797
11.750 1.0618 0.02164 0.01607 0.0239 0.0434 0.9112
12.000 1.0945 0.02233 0.01692 0.0212 0.0427 0.9612
12.250 1.1158 0.02312 0.01774 0.0206 0.0417 1.0000
12.500 1.1279 0.02417 0.01884 0.0213 0.0411 1.0000
12.750 1.1411 0.02517 0.01985 0.0218 0.0400 1.0000
13.000 1.1527 0.02632 0.02101 0.0224 0.0392 1.0000
13.250 1.1619 0.02765 0.02236 0.0230 0.0381 1.0000
13.500 1.1689 0.02919 0.02393 0.0236 0.0373 1.0000
13.750 1.1711 0.03115 0.02594 0.0243 0.0362 1.0000
14.000 1.1842 0.03228 0.02711 0.0246 0.0359 1.0000
14.250 1.1981 0.03335 0.02822 0.0248 0.0353 1.0000
14.500 1.2077 0.03480 0.02972 0.0251 0.0349 1.0000
14.750 1.2187 0.03616 0.03111 0.0253 0.0341 1.0000
15.000 1.2290 0.03761 0.03260 0.0254 0.0334 1.0000
15.250 1.2378 0.03925 0.03428 0.0255 0.0327 1.0000
15.500 1.2460 0.04097 0.03601 0.0255 0.0318 1.0000
15.750 1.2507 0.04307 0.03814 0.0255 0.0309 1.0000
16.000 1.2522 0.04553 0.04065 0.0254 0.0302 1.0000
16.250 1.2647 0.04695 0.04213 0.0252 0.0298 1.0000
16.500 1.2750 0.04861 0.04383 0.0250 0.0291 1.0000
16.750 1.2843 0.05038 0.04566 0.0248 0.0283 1.0000
17.000 1.2912 0.05244 0.04776 0.0244 0.0277 1.0000
17.250 1.2977 0.05458 0.04992 0.0240 0.0267 1.0000
17.500 1.3019 0.05701 0.05237 0.0235 0.0257 1.0000
17.750 1.3054 0.05955 0.05497 0.0229 0.0249 1.0000
18.000 1.3127 0.06170 0.05718 0.0224 0.0242 1.0000
18.250 1.3184 0.06405 0.05958 0.0217 0.0233 1.0000
18.500 1.3217 0.06673 0.06230 0.0209 0.0222 1.0000
18.750 1.3223 0.06980 0.06539 0.0200 0.0211 1.0000
19.000 1.3253 0.07261 0.06827 0.0190 0.0199 1.0000
19.250 1.3256 0.07580 0.07150 0.0179 0.0186 1.0000
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